Airline Transport Pilot, Aircraft Dispatcher, and Flight Navigator

DOCUMENT RESUME

ED 314 618 CE 053 977

TITLE Airline Transport Pilot, Aircraft Dispatcher, and Flight Navigator. Question Book. Expires September 1, 1991. INSTITUTION Federal Aviation Administration (DOT), Washington., D.C. REPORT NO FAA-T-8080-5C PUB DATE 89 NOTE 369p. AVAILABLE FROMSuperintendent of Documents, U.S. Government Printing Office, Washington, DC 20402 (Stock No. 050-007-00820-1: $16.50). PUB TYPE Tests/Evaluation Instruments (160)

EDRS PRICE MF01/PC15 Plus Postage. DESCRIPTORS Aircraft Pilots; *Air Traffic Control; Air Transportation; Aviation Education; *Aviation Technology; Aviation Vocabulary; *Flight Training; *Job Training; Occupational Information; Postsecondary Education; Testing; Test Items IDENTIFIERS *Aircraft Dispatchers; *Flight Navigators

ABSTRACT This question book was developed by the Federal Aviation Administration (FAA) for testing applicants who are preparing for certification as airline transport pilots, aircraft dispatchers, or flight navigators. The publication contains several innovative features that are a departure from previous FAA publications related to air carriar personnel certification written tests: (1) testing materials related to the pilot who seeks to advance to the airline transport pilot level are contained in this book, rather than in the previous two separate books; and (2) the test questions are multiple choice, but have three, rather than four, alternative answers, to allow the use of new scoring techniques. The book has been developed to test applicants in the following knowledge areas: air transport pilot-airplane (in two parts), added rating--airplane, helicopter, added rating--helicopter; aircraft dispatcher; and flight navigator. Extensive appendixes provide statistical and background materials needed to answer the questions, including 157 figures. (Answers to the questions are not included, nor are they published by the FAA.) (KC)

Reproductions supplied by EDRS are the best that can be made * from the original document. FAA-T-8080-5C

AIRLINE TRANSPORT PILOT, AIRCRAFT DISPATCHER, AND FLIGHT NAVIGATOR QUESTION BOOK

U,i DEPARTMENT OF EDUCATION Mc of Educational Research andImprovement ATtONAL RESOURCES INFORMATION CENTER (ERIC) This document has bum reproducedas received from the person or organization originating it. O Minor .;hangs have been made toimprove reproduction duality

Points of vow or opinions stated in this doctr mint do not necessarily represent officio] OEF position or policy US. Department of lionsportation Federal Aviation Administration Expires September 1, 1991

2 BEST COPY AVAILABLE AIRLINE TRANSPORT PILOT, AIRCRAFT DISPATCHER, AND FLIGHT NAVIGATOR

19P9

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION Aviation Standards National Field Office PREFACE

This question book has been developed by the Federal Aviation Administration (FAA) for testing applicants who are preparing for certification as airline transport pilots, aircraft dispatchers, or light navigators.

The pulecation contains several innovative features which are a departure from previous FAA issuances related to air carrier airman certification written tests. These new features are:

1.Testing materials related to the pilot who seeks to advance to the airline transport pilot level are contained in this book. These testing materials are appropriate for testing pilots who have had training or actual experience in flight operations conducted under either FAR Part 121 or FAR Part 135. This feature eliminates the publication of two separate books which contained a significant amount of redundant materials. The combined questii3n book contains test items covering all the written test variations formerly covered in the two books. The airline transport pilot applicant may still request a test related to his or her particular training or experience as related to operations conducted under FAR Part 121 or FAR Part135.

2. The test questions contained in this publication are all multiple-choice type, a standard practice for all FAA certification written tests. However, the test questions contained in this book have been developed to offer the applicant three alternative answens, rather than the four-answer format used on other FAA written tests. This change has been adopted to allow the use of new scoring analysis techniques.

This question book has been developed to test applicants in the following knowledge areas:

Airline Transport Pilot (FAR Part 121) Airplane Airline Transport Pilot (FAR Part 135) Airplane Airline Transport Pilot (FAR Part 135) Added Rating-Airplane Airline Transport Pilot (FAR Part 135) Helicopter Airline Transport Pilot (FAR Part 135) Added Rating-Helicopter Aircraft Dispatcher Flight Navigator

This publication is issued as FAA-T-8080-5C, Airline Transport Pilot Aircraft Dispatcher, and Right Navigator Question Book, and is available to the public from:

Superintendent of Documents U.S. Government Printing Office Washington, DC 20402

or from U.S. Government Printing Office bookstores located in major cities throughout the United States.

The questions included in this publication are predicated on regulations, principles, and practices that were valid at the time of publication. The question selection sheets prepared for use with this question book are security items and are revised at frequent intervals.

The FAA does NOT publish, supply, or make available the correct answers to questions included in this book. Students should detennine the answers by research and study, by working with instructors, or by attending ground schools. The FAA is NOT responsible for either the content of commercial reprints of this book or the accuracy of the answers they may list.

Comments regarding this publication should be directed to:

U.S. Department of Transportation Federal Aviation Administration Aviation Standards National Field Office Examinations Standards Branch Operations Standards Section, AVN-131 P.O. Box 25082 Oklahoma City, OK 73125

Iii 4 Contents

Page

Preface W Contents. v General instructions. ix Introduction to the Airline Transport Pilot, Aircraft Dispatcher, and Flight Navigator Question Book. xi Questions 1

Appendix 1

Subject Matter Knowledge Codes 1 Appendix 2

Legend 1.-instrument Approach Procedures Chart (Approach Lighting Systems) 1 Legend 2.-General information and Abbreviation & 2 Legend 3.-instrument Approach Procedures Chart (Planvlew) 3 Legend 4.-Instrument Approach Procedures Chart (Profile) 4 Legend 5.-instrument Approach Procedures Chart (Airport Diagram)... 5 Wand O.-Rated-Descent Table.... 6 Legend 7.-Rate-of-Climb Table 7 Legend 8.-Inoperative Components or Visual Aids Table 8 Legend 9.-Instrument Approach Procedures Explanation of Terms 9 Legend 10.-Directory Legend (Sample) 10 Lewd ft-Directory Legend 11 Legend 12.- Directory Legend (Codes) 12 Legend 13.-Directory Legend (Runway Data) 13 Legend 14.-Directory Legend (Visual Gedeslope Indicator) 14 Legend 15.- Directory Legend (Communications) 15 Legend 18.- Directory Legend (Radio Aids to Navigation) 18 Legend 17.-Directory Legend (Frequency Pairing Plan and MLS Channeling) 17 Legend 18.-En Route Lo- Altitude - U.S 18 Legend 19.-Air Traffic Services and Airspace informa ton 19 Legend 20.--HeNcopter Route Chart 20 Legend 21.-Helloopter Route Chart. 21 Legend 22.-Akports. 22 Legend 23.-IFR En Route High Altitude Chart. 23 Legend 24.-Hazardous Materials Table (CFR 49 Part 172) 24 Legend 25.-Hazardous Materials Table (CFR 49 Part 172) (Cont'd) 25 Legend 28.-Hazardous Materials Table (CFR 49 Part 172) (Cont'd) 28 Legend 27.- Excerpt from CFR 49 Part 175 27 Legend 28.-Excerpt from CFR 49 Part 175 28 Legend 29.-Excerpt from CFR 49 Part 175 29 Legend 30.- Excerpt from CFR 49 Part 175 30 Legend 31.-Excerpt from CFR 49 Part 175 .31 Legend 32.-Excerpt from CFR 49 Part 175 32 Legend 33.-Excerpt from CFR 49 Part 175 33 Legend 34.-Excerpt from CFR 49 Part 175 34 Legend 35.-Excerpt from CFR 49 Part 175 35 Legend 38.-Excerpt from CFR 49 Part 175 38 Legend 37.-Excerpt from CFR 49 Part 175 37 Legend 38.-PIREP 38 Legend 39.-Key to Radar Summery Chart. 39 Appendix 3

Figure 1.-Flight Plan/Flight Log 1 Figure 2.-FLIPR Two Departure (Pilot Nay) 2 Figure 3. -Arlin Five Arrival/LOC BC RWY 28L. 3 Figure 4.-Power Plant Visual RWY 28L. 4

v 5 Contents-Continued

Figure 5.-IFR En Route High Altitude Chart Segment 5 Figure 5A.-IFR En Route High Altitude Chart Segment 8 Figure 6.-Right Plan/Right Log 7 Figure 7.-Tucson Two Departure (Pilot Nay) 8 Figure 8. -Downs Two Arrival (Downe.Downe2) 9 Figure 9.-ILS RWY 25L (CAT II)- Los Angeles International (LAX) 10 Figure 10.--Flight Plan/Right Log 11 Figure 11.-En Route Low Altitude Chart Segment 12 Figure 12.-Flight Plan/Flight Log 13 Figure 13.-Buffalo One Departure (Vector)- Buffalo/ Greater Buffalo Intl 14 Figure 14.-IFR En Route High Altitude Chart Segment 15 Figure 15.-Flight Phut/Right Log 18 Figure 16.-Canal Three Departure (Vector)- Chicago Midway 17 Figure 17.-RNAV RWY 32 and Excerpt (BUF) 18 Figure 18.-Helicopter Route Chart 19 Figure 19. -Flight Plan/Right Log 20 Figure 20.-IFR Area Chart Segment 21 Figure 21.-IFR En Route Low Altitude Chart Segment 22 Figure 22.-Akport/Fadlity Directory Excerpts 23 Figure 23.-Cu gar Four Arrival (Cugar.Cugar4)/VOR/DMERWY 32R (IAN) 24 Figure 24.-Flight Plan/Right Log. 25 Figure 25.-Cyter VOR/DME 117' (HUM) and Excerpt fromA/FD 26 Figure 26.-LDA/DME-2 RWY 18 (TVL) and Excerpt from A/FD 27 Figure 27.-LOC BC RWY 14 (SBY) and Excerpt fromA/FD 28 Figure 28. -MLS RWY 19L (ICT) and Excerpt from A/FD 29 Figure 29.-NDB RWY 15 (CHS) and Excerpt from A/FD 30 Figure 30.-SOF RWY 31 (NC14) and Excerpt from A/FD 31 Figure 31.-CM Radar Instrument Approach Minimums 32 Figure 32.-13-727 Loading 33 Figure 33.-13-727 Loading 33 Figure 34.-13-727 Loading 33 Figure 35.-Table of Weights and Limits 34 Figure 36.-Loading Tables. 35 Figure 37.-DC-9 Weight Shift 36 Figure 38.-Beech 1900 Loading Passenger Configuration 36 Figure 39.-Beech 1900 Loading Cargo Configuration V Figure 40. - Airplane- Loading Data. 38 Figure 41.--CG Envelope and Cargo Loading Data. 39 Figure 42.-Airplane- Weights and Moments - Baggage 40 Figure 43.-Airplane- Weights and Moments - Occupants 41 Figure 44.-Density Variation of Aviation Fuel 42 Figure 45.-Airplane- Weights and Moments - Usable Fuel 43 Figure 48.-Beech 1900 Loading Limitations 44 Figure 47.-Bell 214 ST Loading 44 Figure 48.-Bell 214 ST Weight Shift and Limits 45 Figure 49.-Helicopter- Loading Data. 46 Figure 50.-Helicopter- Weights and Moments - Crew, Passengers, and Baggage 47 Figure 51.-Helicopter - Weights and Moments - Usable Fuel 48 Figure 52.--Helicopter- Lateral CG Envelope 49 Figure 53.-Helicopter- Longitudinal CG Envelope 50 Figure 54.-Altimeter Setting to Pressure Altitue 51 Figure 55.-DC-9 Takeoff 52 Figure 58.-Takeoff Speeds. 53 Figure 57.-13-727 Takeoff 54 Figure 58.-Takeoff Performance Figure 59.-B-737 Takeoff 53 58 Figure 80.-B-737 En Route Climb 58 Figure 81.-Takeoff Performance 57 Figure 62.-En Route Climb 280/.70 ISA. 58 Figure 83.-En Route Climb 280/.70 +10' C 53 Figure 64.-8-737 Climb and Cruise Power 80

vi Contents-ContInued

Figure 65. -DC-9 En Route Climb 80 Figure 66.-Climb and Cruise Power 61 Figure 67.-High-Speed Climb Schedule 62 Figure 88.-Long-Range Climb Schedule 63 Figure 89.-Flight Planning at .78 Mach Cruise 64 Figure 70.- Turbulent Air RPM 64 Figure 71.-Flight Planning .78 Mach indicated 85 Figure 72.-Flight Planning at .74 Mach Cruise 66 Figure 73.- Turbulent Air Penetration 86 Figure 74.-Abbreviated Flight Planning 67 Figure 75.-DC-9 Alternate Planning ee Figure 76.-B-727 Holding 68 Figure 77.-B-737 Holding. 88 Figure 78.- Alternate Planning Chart. ea Figure 79.-Holding Performance Chart 69 Figure 80.-Holding Performance Chart 70 Figure 81.-Fuel Dump Time 71 Figure 82.-B-737 Drift-Down 71 Figure 83.-Descent Performance 71 Figure 84.-Drift-Down Performance Chart. 72 Figure 85.-Descent Performance Chart. 73 Figure 86.-13-727 Landing. 74 Figure 87.--Landing Performance Chart 74 Figure 88.-Normal Landing - Dry Runway 75 Figure 89.-Normal Landing - Wet Runway.. 78 Figure 90.-Normal Landing - Icy Runway 77 Figure 91.-Normal Landing Distance Comparison 78 Figure 92.-Landing Thrust - 110,000 Pounds 79 Figure 93.-Landing Thrust - 140,000 Pounds 80 Figure 94.-Minimum Takeoff Power at 1700 RPM 81 Figure 95.-Takeoff Distance - Flaps Takeoff 82 Figure 96.-Accelerate-Stop - Raps Takeoff 83 Figure 97.-Beech 1900 Climb Table 84 Figure 98.-Climb - Two Engines - Flaps Up 84 Figure 99.-Climb - One Engine In oreerative 85 Figure 100.-Time, Fuel, and Distance to Cruise Climb 88 Figure 101.-Beech 1900 Service Ceiling 87 Figure 102.-Beech 1900 Cruise 87 Figure 103.-Service Ceiling - One Engine Inoperative 88 Figure 104.-Recommended Crui' Power - ISA +10' C 89 Figure 105.-Recommended Cruise Power - ISA 90 Figure 106.-Recommended Cruise Power - ISA -10' C 91 Figure 107.-Time, Fuel,and Distance to Descend 92 Figure 108.-Beech 1900 Landing 93 Figure 109.-Normal Landing Distance - Flaps Landing 94 Figure 110.-Power Assurance Check. 95 Figure 111.-Hovering Ceiling - In Ground Effect 96 Figure 112.-Hovering Ceiling - Out of Ground Effect. 97 Figure 113.-Takeoff Distance Over 50-Foot Obstacle 98 Figure 114.-Twin-Engine Climb Performance 99 Figure 115.--Single-Engine Climb Performance 100 Figure 116.-Airspeed Limit 101 Figure 117.-Single-Engine Landing Distance Over 50-Foot Obstacle 102 Figure 118.-Wind Component Chart 103 Figure 119.-Microburst Section Chart 104 Figure 120.-Surface Aviation Weather Report 105 Figure 121.-Stxface Aviation Weather Report 106 Figure 122.-Terminal Forecast 107 Figure 123.-Area Forecast 108 Figure 124.-Convective Slgmet. 109 Figure 125.-Winds and Temperatures Aloft Forecast. 110

vii 7 Contents Continued

Figure 128. Weather Depiction Chart 111 Figure 127. -Radar Summary Chart. 112 Figure 128.-SignMowit Weather Prognostic Chart. 113 Figure 129. -600 MS Analysis Heights/Temperature Chart 114 Apure 130.-300 MB Analysis Heights/isotache Chart. 115 Figure 131.-200 MB Analysis Heights/Isotacha Chart. 116 Figure 132A.-Tropopause Pressure 117 Figure 13213.-Tropopause Streams/lsotachs. 118 Figure 132C.-High-Level Significant Weather Chart. 119 Figure 132D.-Tropopause Pressure/VHS 120 Figure 133A.--Severe Weather Outlook (AC) 121 Figure 1338. -severe Weather Outlook (AC) 122 Figure 134.-STARS, July- December 123 Figure 135.-Greenwich Day 282 124 Figure 136.--Greermich Day 263 125 Figure 137.-Greenwich Day 263 128 Figure 138.-Polaris (Pole Star) Table 127 Figure 139.-Sedant Altitude Corrections 128 Figure 140.-LAT 32'N 129 Figure 141.-LAT 28'N 130 Figure 142.-Precession and Nutation Correction 131 Figure 143. - Polaris Correction 132 Figure 144.-Refraction and Coriolis. 133 Figure 145. -Declination (0°- 14') LAT 25' 134 Figure 148.-DecInadon (Cr- 141 LAT 25' 135 Figure 147.-Declination (0'- 14') LAT 27' 138 Figure 148. - Declination (15°- 291 LAT 276 137 Figure 149.-Deciination (Os- 141 LAT 31' 13$ Figure 150. - Declination (0'- 14') LAT 32' 139 Figure 151. -- Declination (15'- 29') LAT 32' 140 Figure 152.-Tabulated Altitude Correction Table 141 Figure 153. - Altitude Correction for Position Table 142 Figure 154.-Navigation Chart. 143 Figure 155.-Navigation Chart. 144 Figure 156.-Navigation Chart. 145 Figure 157.-Navigation Chart. 148

vill 8

--- GENERAL INSTRUCTIONS MAXIMUM TIME ALLOWED FOR TEST: 6 HOURS

TEST MATERIALS Materials to be used with this question book when used for airman testing: 1. AC Form 8080.3, Airman Written Test Application, which includes the answer sheet 2. Question selection sheet which identifies the questions to be answered. 3. Plastic overlay sheet which can be placed over performance charts for plotting purposes.

TAKING THE TEST

1. Read the instructions on page 1 of AC Form 8080.3, and complete page 4 of the form. 2. The question numbers in the question book are numbered consecutively beginning with number5001. Refer to the question selection sheet to determine which questions to ar ewer. 3. For each item on the answer sheet, find the appropriate question in the question book. 4. Mark your answer in the space provided for that item on the answer sheet 5. Miscellaneous reference materials are in appendix 2. 8. The supplementary material required to answer the questions will be found in appendbc 3. 7, Read each question carefully and avoid hasty assumptions. Do not answer until you understand thequestion. Do not spend too much time on any one question. Answer all the questions that you readily know and thenreconsider those you find difficult Be careful to make necessary conversions when working with temperatures, speeds,and distances. If a regulation, chart, or operations procedure is changed after this question book is printed, youwill receive credit for the affected question until the next question book revision. Comments regarding this pubNcation should be directed to: U.S. Department of Transportation Federal Aviation Administration Aviation Standards National Field Office Examinations Standards Branch Operations Standards Section, AVN-131 P.O. Box 25082 Oklahoma City, OK 73125

THE MINIMUM PASSING GRADE IS 70

WARNING

161.37 Written teats: aseating or other (6)Intentionallycause,assist,or =authorized conduct. participate in any act prohibited by this paragraph. (a)Exceptasauthorizedbythe (b) No person whom the Administrator Administrator, no person may finds to have committed an act..thib- (1) Copy, or intentionally remove, a ited by paragraph (a) of this lection is written test under this part; eligible for any airman or ground in- (2) Give to another, or receive from structor certificde or rating, or to take another, any part or copy of that test; any test there ore, under this chapter for (3) Give help on that test to, or receive a period of 1year after the date of help on that test from, any person during that act. In addition, the commission of theperiodthattestisbeinggiven; that act is a basis for suspending or (4) Take any part of that test in behalf revoking any airman or ground instruc- of another person; tor certificate or rating held by that (5) Use any material or aid during the person. period that test is being given; or

Ix 9 -k,

INTRODUCTION TO THE AIRLINE TRANSPORT PILOT, AIRCRAFT DISPATCHER, AND FLIGHT NAVIGATOR QUESTION BOOK

This question book presents the FM written tests to the 1. Answer each question In accordance with the latest applicants. The book consists of questions on subject areas regulations and procedures. pertaining to the airline transport pilot, aircraft dispatcher, 2. Read each question carefully before looking at the and flight navigator certificates. This question book is possible answers. You should dearly understand scheduled for revision each 24 months, and associated the problem before attempting to solve it question selection sheets will be revised periodically as 3. After formulating an answer, determine which of required. the alternatives most near* corresponds with that answer. The answer chosen should completely At an FM testing center or an FM designated written test resolve the problem. examinees facility, the applicant is issued a "clean copy' of 4. From the answers given, it may appear that there is this question book, an appropriate question selection ghost more than one possible answer; however, there is which indicates the specific questions to be answered, and only one answer that is correct and complete. The AC Form 8080-3, Airman Written Test Application, which other answers are either incomplete or are derived oontelne the answer sheet. The question book contains all from popular misconceptions. the supplementary material required to answer the ques- 5. If a certain question is difficult for you, it is best to tions. This materialwillbe found in appendix 2 and proceed to other questions. After the less difficult appendbc 3. questions have been answered, return to those which gave you difficulty. Be sure to indicate on the Qaestions and Scoring question selection Silget the questions to which you wish to return. Answers to questions listed on the question selection sheet 6. When solving a computer problem, select the should be marked on the answer sheet of AC Form 8080-3. answer nearest your solution. The problem has Directions should be read carefully before beginning the been checked with various types of computers; test. Incomplete or erroneous personal information entered therefore,if you have solved itcorrectly, your on this form delays the scoring process. The answer sheet answer will be closer to the correct answer than to is sent to the Mike Monroney Aeronautical Center In any of the other choices. is scored by computer. The Oklahoma City where it 7. To aidInscoring, enter personal data in the applicant will then be issued an AC Form 8080-2, Airman appropriate spaces on the test answer sheet in a Written Test Report This report must be presented for a complete and legible manner. Enter thetest flight test or for retesting in the event of written test failure. number printed on the question selection sheet The applicant's AC Form 8000-2 will list the subject matter knowledge codes for the knowledge areas in which the RetestingFAR Section 61.49 applicant is found to be deficient The written test subject matter knowledge codes, which list these knowledge areas Applicants who receive a failing grade may apply for by code, are located in apppendbc I of this question book. retesting

Taking the Test 1. after 30 days from the date the applicant failed the test; or The test may be taken at FM testing centers, FM written 2. In case of the first failure, the applicant may apply test examiners' facilities, or other designated places. After for retesting before the 30 days have expired upon completing the test, the applicant must surrender the issued presenting a written statement from an authorized question book, question selection sheet, answer sheet, and instructor certifying that the instructor has given any papers used for computations or notations, to the ground instruction to the applicant and finds the monitor before leaving the test room. applicant competent to pass the test.

When taking the test,the applicant should keep the The AC Form 8080-2, Airman Written Test Report, must be following points in mind: presented for the practical test, or for retesting In the event of written test failure.

x110 QUESTIONS

5001. What is an area identified by the term stopway? 5009. What is the correct symbol for minimum unstick speed? 1-An area, at least the same width as the runway, capable of supporting an airplane during a normal takeoff. 1-Vuu. 2-An area designated for use In decelerating an aborted 2-Vuu. takeoff. 3'' VFC. 3-An area,not as wide as the runway, capable of supporting an airplane during a normal takeoff. 5010. Which is a definition of Vs speed?

5002. Regulations concerning the operational control of a 1-Takeoff decision speed. flight refer to 2-Takeoff safety speed. 3-Minimum takeoff speed. 1-the specific duties of any required crewmember. 2-exercising authority over initiating, conducting, or termi- 5011. When a temporary replacement is received for an nating a flight airman's medical certificate, for what maximum time is this 3-exercising the privileges of pilot in command of an document valid? aircraft 1-30 days. 5003. What is a definitionof the term crewmember? 2-80 days. 3-90 days. 1-Only a pilot, flight engineer, or flight navigator assigned to duty in an aircraft during flight time. 5012. Unless otherwise authorized, the pilot in command is 2-A person assigned to perform duty in an aircraft during requiredtohold a typerating when operating any flight time. 1-aircraft that is certificated for more than one pilot 3-Any person assigned to duty in an aircraft during flight 2-aircrafthaving agrossweightof morethan except a pilot or flight engineer. 12,500 pounds. 5004. What is the name of a plane beyond the end of a 3--multiengine aircraft having a gross weight of more than runway which does not contain obstructions and can be 8,000 pounds. considered when calculating takeoff performance of turbine- 5013. The pilot in command is normally required to hold a powered aircraft? type rating when operating which of the following? 1-Clearway. 1-Any turbojet-powered airplane. 2-Stopway. 2-Any airplane which has a gross weight of 6,000 pounds 3-Obstruction clearance plane. Ofmore. 5005. The minimum steady flight speed or stalling speed in 3-Any multiengine airplane whichisoperated under the landing configurationis represented by the symbol interstate commerce. 1-Vs. 5014. What is the lowest HAT for which a Category II 2-VE. applicant can be certified during the first 6 months of 3-V,0. Category II operations?

5008. Which is the correct symbol for the stalling speed or 1-100 feet AGL the minimum steady flight speed at which the airplane is 2-150 feet AGL controllable? 3-200 feet AGL 1-Vs0. 5015. A Category II ILS pilot authorization, when originally 2-Vs. issued, is normally limited to 3-VE. 1-Category II operations not less than 1800 RVR and a 5007. Which is the correct symbol for design cruising 150-foot OH. speed? 2-pilots who have completed an FAA-approved Category II training program. 1-Vu. 3-Category II operations not less than 1200 RVR and a 2-Vs. 100-foot DH. 3-VW. 5018. When may a Category II ILS limitation be removed? 5008. Which speed symbol indicates the maximum operating limit speed for an airplane? 1-When three ILS approaches have been completed to a 150-foot decision height 1-Vsu. 2-When six ILS approaches to Category II minimums have 2-Vuu/Muu. been completed in the past 8 months. 3-Vw/Mw. 3-120 days after issue or renewal.

11 5017. What minimum Instrument time in thepast 6 months 5022. Within the past 6 months a pilot has accomplished: meets the second-In-command requirement tomaintain IFR currency In a helicopter? Two approaches in a helicopter Two approaches in an airplane 1-3 hours of actual or simulated timein the same type Two approaches in a simulator helicopter. 2-3 hours of actual or simulated IFRin a helicopter. What additional approaches, If any, must that pilotperform 3-3 hours of actual or simulated IFR Ina helicopter and to act as second in command on an IFR helicopter flight? 3 hours In an approved simulator. 1None. 5016. What minimum conditionsare necessary for the 2One in a helicopter. Instrument approaches required for secondin command IFR 3One in either a helicopter or an airplane. currency In a helicopter? 5023. What instrument flight timemay be logged by a 1Three must be made in a helicopter. second in command of an aircraft requiring two pilots? 2Three must be made in a rotorcraft category. 1All of the time the second in command 3All may be made In an airplane, helicopter,or approved is controlling the simulator. airplanesolely by referencetoflightinstruments. 2One-half the time the flight ison an IFR flight plan. 5019. Within the past 6 months a pilot hasaccomplished: 3One-half the time the airplane is in actual IFR conditions. One approach in a helicopter 5024. What Instrument flight timemay be logged by the Two approaches in an airplane second in command of a two-pilot air taxi flight? Two approaches in an approved simulator 1All of the time the second in command iscontrolling the What additional approaches, If any, must thepilot perform to airplanesolely by reference toflightinstruments. act as second in command on an IFR helicopterflight? 2One-half the time the *light ison an IFR flight plan. 1None. 3All of the time the airplane is in actual IFR conditions. 2One approach in an airplane, helicopter,or approved 5025. To satisfy the minimum required instrument experi- rrimulatoc ence for IFR operations, a pilot must accomplish during the 3-.Two approaches In a helicopter andone approach in an past 6 months at least approved simulator. 1six instrument approaches and 6 hours of instrument 5020. A pilot, acting as second in command,successfully time, 3 of the 6 hours in flight in the category of aircraft completes the instrument competency checkspecified in to be flown. FAR Part 61. How long does this pilotremain current if no 2six instrument approaches, three of which must be in the further IFR flights are made? same category and class of aircraft to be flown, and 6 hours of iristrument time in any aircraft 1-12 months. 2-90 days. 3six instrument approaches and 6 hours of instrument time in any aircraft 3-6 months. 5026. To be eligible for the practical test for the renewal of 5021. Within the past 6 months a pilot has accomplished: a Category II authorization, what recent instrument approach experience is required? 1 hour actual IFR and 1 hour simulated IFRin a helicopter 1Within the previous 6 months, six ILS approaches, three 2 hours actual IFR in an airplane of which may be flown to the Category I DH by 1 her in an approved simulator use of an approach coupler. What additional Instrument time,ifany, must that pilot 2Within the previous 6 months, six ILS approaches flown acquire to act as second in commandon an IFR helicopter by use of an approach coupler to the Category I DH. flight? 3Within the previous 12 calendar months, threi; IS approaches flown by use of an approach coupler to the 1None. Category II DH. 2-1 her actualorsimulated IFRina helicopter. 3-1 hour actual or simulated IFR Inan aircraft

12 2 Int A flight requiring two pilots is scheduled on August 1. 503.t. A commercial pilot has DC-3 and DC-9 type ratings. Both the pilot in commend and the second in command A 'Bight test is completed for an Airline Transpon Pilot have RIM-Class Medical earnest's dated February 28. Cietificateina B-727. What pilotprivileges may be Priorto the ucheduledflight,thepilotin command (atomised? 1end second in command must hold certificates appropri- 1ATP-8-727 and DC-3; CommercialDC-9. ate for the fight 2ATPB-727 only; CommercialDC-9 and DC-3. 2must obtain a new First-Class Medical Ceftfficate; the 3ATPB-727 And DC-9; CommercialDC-3. second in cu mend must have a new medical certifi- 5034. A commercial pilot has a type rating in a B-727 and cate, but a Second-Class MedicalOertificate is ade- B-737. A flight test Is completed in a B-74"1 for the Airline quate. 3must obtain a new First-Class Medical Certificate; the Transport Pilot Certificate. What pilot privileges may be second In command's certificate 1adequate. exercised regarding these airplanes? 1CommercialB-737; ATP-8-727 and B-747. MK To be eligible for the practical test for the original 2ATPB-747; CommercialB-72? and B-737. issue of a Category II authorization, what recent experience 3ATP-0-747, B-727, and B-737. N required? 1Within the previous 8 months, skit ILS approaches flown 5035. To serve as flight navigatur, a person must possess manually tt. the Category I DM. 1a current Flight Navigator Certificate only. 2Within theprevious12 calendar months,sixILS 2a current Flight Navigator Certificate and at least a approaches flown by use of an approach coupler to the Second-Class Medical Certificate. Category I or Category II DH. 3a current Third-Class Medical Certificate and Airline 3Within the previous 8 months, six ILS approaches, three Transport Pilot Certificate. of which may be flown to the Category I DH by use of an approach coultier- 5038. A Flight Navigator Certificate remains ineffect 0028. What Is the minimum number of instrument ap- 1for 2 years. proaches required to act as pilot in command uncle!FR 2for 12 calendar months. oondllons? 3until surrendered, suspended, or revoked. 1Six in any approved instrument ground trainer or aircraft 5037. How many hours of satisfactory flight navigation within the past 8 months. experience must an applicant have logged to apply for a 2Six, at least three of which must be in an aircraft, within Flight Navigator Certificate if the applicant has no pilot time? the pest 8 months. 3Six in el aircraft, at least three of which must be in the 1-100 hours. elms category, within the past 8 months. 2-200 hours. 3-500 hours. BOK When an airline transport pilot Is instructing other pilots in at transportation service, instruction is restricted to 5038. How many hours of satisfactory flight navigation experience must an applicant have logged to apply for a 1those aircraft In which the pilot holds a category, class, Flight Navigator Certificate if the applicant has 500 hours of and type rating. crot. -country flight time as pilot, of which atleast 100 hours 2a maximum of 30 hours in any 7-day period. were at night? 3a school conducted by a certificatedaircarrier. 1-100 hours. 8081. What restriction Is Imposed regarding flight instruction 2-200 'lours. of other pilots In air transportation service by an airline 3-500 nours. transpod pilot? 5039. If an applicant for a Flight Navigator Certificate fails 1-30 hours In any 7-day period the flight portion of the practicaltest, when may the 2-7 hates in any 1-day period. applicant be retested? 3-38 hours in any 7-day period. 1At the end of a 30-day period or afterreceiving 8032. What maximum hours a day may an airline transport additional in-flight instruction. pilotinstruct otherpilotsinair transportation service? 2After 10 hours of flight instruction. 3After 5 hours of ground instructioninnavigation. 1-8 Sours. 2-8 hours. 5040. What docurnent(s) must be in a person's possession 3--10 hours. for that person to act as a flight navigator? 1Current FlightNavigatorCertificateand a current Second-Class (or higher) Medical Certificate. 2Currer .light Navigator Certificate and a valid passport 3Third-Class Medical Certificate and cur+ ant Flight Naviga-

k tor Certificate.

313 1041. A turbine-engine-powered or large airplane isre- 5050. When proceeding to the alternate airport, which quired to enter an Airport Traffic Area at an altitude of at minimums apply? least 1The IFR alternate minimums section in front of the 1-1,500 feet AGL NOAA IAP book. 2-2,000 feet AOL 2-2000-3 for at least 1 hour before until 1 hour after the 3-3,000 feet AOL ETA. 3The actual minimums shown on the IAP chart for the 5042. What is the maximum indicated airspeed a recipro- airport cating-engine-powered airplane may be operated within a TCA? 5051. The !abilitycriteriafor a particularinstrument 1-180 knots. approach procedure is RVR 40. What minimum ground 2-230 knots. visibility may be substituted for the RVR value? 3-250 knob. 1-5/8 SM. 2-3/4 SM. 1043. At what maximum indicated airspeed can a B-727 3-7/8 SM. operate within a TCA without special ATC authorization? 1-230 knots. 5052. The prescribed visibility criteria of RVR 32 for the 2-250 knots. runway of intended operation is not reported. What minimum 3-275 knots. ground visibility may be used instead of the RVR value? 1-3/8 SM. 5044. At what maximum indicated airspeed may a recipro- 2-5/8 SM. cating-engine-powered airplane be operated withinan 3-3/4 SM. Airport Traffic Area? 1-158 knots. 5053. What minimum ground visibility may be used instead 2-180 knots. of a prescribed visibility criteria of RVR 18 when that RVR 3-200 knots. value is not reported? 1-1/4 SM. 5045. What is the maximum indicated airspeeda turbine- 2-3/4 SM. pcweristo. aircraft may be operated below 10,000 feet MSL? 3-3/8 SM. 1-288 knots. 2-250 knots. 5054. While in IFR conditions a pilot experiences two-way 9-230 knots. radio communications failure, which route should be flown in the absence of an ATC assigned route or a route ATC has 5048. At what maximum indicated airspeedcan a recipro- advised to expect In a further clearance? cating-engine airplane operate in the airspace underlyinga 1The most direct route to the filed alternate airport. Terminal Control Area? 2An off-airway route to the point of departure. 1 -180 knots. 3The route filed in the flight plan. 2-200 knots. 3-230 knots. 5055. What altitude and route should be used if the pilot is flying in IFR weather conditions and has two-way radio 5047. A pilot of a turbine-powered airplane should climbas communications failure? rapidly as practicable after taking off to what altitude? 1Continue on the route specified in the clearance and fly 1-1,000 feet AOL the highest of the following: the last assigned altitude, 2-1,500 feet AOL altitude ATC has informed the pilot to expect, or to the 3 -5,001 feet AOL MEA. 2Descend to MEA and, if clear of clouds, proceed to the 5048. What action should a pilot take when a clearance is nearest appropriateairport.Ifnot clear of clouds, received from ATC that appears to be contrary toa maintain the highest of the MEA's along the clearance regulation? route. 3Fly the most direct route to the destination, maintaining 1Read the clearance back in Its entirety. the last assigned altitude or MEA, whichever is higher. 2Request a clarification from ATC. 3Do not accept the clearance. 5048. Which facility may be substituted for the middle marker during a Category I ILS approach? 1VOR/DME FIX. 2Survelliance radar. 9Compass locator. 14 4 5062. A pilot Is operating outside of controlledairspace. If 5066. After experiencing two-way radio communications VFR flight failure en route, when should a pilot begin the descent for existing weather conditions are below those for filed and an ATC clearance the instrument approach? an IFR flight plan must be received prior to 1Upon arrival at any initial approach fix for the instrument minimums. approach procedure but not before the flight plan ETA 1takeoff if weather conditions are below IFR as amended by ATC. 2entering controlled airspace. 2Upon arrival at the holding fix depicted on the instrument 3entering IFR weather conditions. approach procedure at the corrected ETA, plus or minus 5063. What minimum altitude should ahelicopter maintain 3 minutes. 3At the primary initial approach fix for the instrument while en route? smooch procedure at the ETA shown on the flight plan 1Over congested areas such as towns. no lowerthan or the EFC time, whichever is later. 1,000 feet over the highest obstacle within ahorizontal radius of 2,000 feet of the helicopter. 1057. If a pilot is being radar vectored In IFR conditions 2That specifically prescribed by the air carrierfor the and loses radio communications with ATC, what action operation. should be taken? 3That prescribed by the Administrator. 1Fly directly to the next point shown on the IFR flight plan 5064. According to FAR Part 91, when takeoffminimums and continue the flight are not prescribed for a civil airport,what are the takeoff 2Squawk 7700 and climb to VFR On Top. minimums under IFR for a single-engine helicopter? 3Fly direct to a fix, route, or airway specified in the vector clearance. 1-1/2 SM visibility. 2-1 SM visibility. 5066. A pilot is flying In IFR weather conditions and has 3-1200 RVR. two-way radio communications failure. What altitudeshould be used? 5065. According to FAR Part 91, whentakeoff minimums airport, what are the takeoff 1Last assigned altitude, altitude ATC has advised to are not prescribed for a civil minimums Jr.der IFR for a multiengine helicopter? expect or the MEA, whichever is highest r;- 2An altitude that is at least 1,000 feet above the highest 1-1 SM visibility obstacle along the route. 2-1/2 SM visibility. 3A VFR altitude that is above the MEA for each leg. 3-1200 RVR.

5059. A pilot is holding at an Initial approach fix after having 5066. When takeoff minimums are notprescribed for a civil experienced two-way -do communications failure. When airport, what are the takeoff minimumsunder IFR for a should that pilot begin descent for the instrument approach? three-engine airplane? 1At the EFC time, if this is within plus or minus 3 minutes 1-1 SM. of the flight plan ETA as amended by ATC. 2-1/2 SM. 2At flight plan ETA as amended by ATC. 3-300 feet and 1/2 SM. 3At the EFC time as amended by ATC. 5067. If being radar vectored to the finalapproach course 5060. Unless otherwise prescribed, what is the rule regard- of a published instrument approach thatspecifies "NO PT," ing altitude and course to be maintained by a helicopter the pilot should during an off-airways IFR flightover non-mountainous be executed. terrain? 1advise ATC that a procedure turn will not 2not execute the procedure turnunless specifically 1-1,000 feet above the highest ,3bstacle within 5 statute cleared to do so by ATC. miles of course. 3execute a holding pattern type procedure turn. 2-2,000 feet above the highest obstacle within 5 statute miles of course. 5066. When must the pilotinitiate a missed approach 3-1,500 feet above the highest obstacle within a horizontal procedure from an ILS approach? distance of 3 statute miles of course. 1At the DH when the runway is notclearly visible. 6061. Unless otherwise prescribed, what is the rule regard- 2When the time has expired after reachingthe DH and ing altitude and course to be maintained by a helicopter the runway environment Is not clearly visible. the intended during an IFR off-airways flight over mountainous terrain? 3At the DH, if the visual references for runway are not distinctly visible oranytime thereafter that 1-1,000 feet above the highest obstacle within a horizontal visual reference is lost distance of 5 statute miles of course. 2-2,500 feet above the highest obstacle within a horizontal distance of 3 nautical miles of course. 3-2,000 feet above the highest obstacle within 5 statute miles of course. 15 5 MN. Assuming that all ILS components are operating and 6076. What action should be taken if one of the two VHF the required visual referencesare r established, the radios fail while IFR in controlled airspace? missed approach should be initiatedupon 1Notify ATC immediately, 1arrival at the OH on the glide slope. 2Squawk 7600. 2arrival at the visual descent point 3Monitor the VOR receiver. 3-- expiration of the time listedon the appruach chart for missed approach. 5077. What action is necessary when a partial loss of ILS receiver capability occurs while operatingin controlled 5070. What action should be taken whena pilot is "cleared airspace under IFR? for approach" while being radar vectoredon an unpublished route? 1Continue as cleared and file a written report to the Administrator if requested. 1Descend to minimum vector altitude. 2If the aircraft is equipped with other radios suitable for 2--Remain at last assigned altitude until gtstablist:ed on a executing an instrument approach, no further action is published route segment. necessary. 3Descend to initial approach fix altitude. 3Report the malfunction immediately to ATC. 5071. Under which condition may a pilot descend below OH 5078. During an emergency, a pilot in command doesnot or MDA when using the ALSF-1 approach light systemas deviate from a FAR rule but is given priority by ATC. To the necessary visual reference for tho intended runway? whom or under what condition is the pilot required tosubmit a written report? 1Under no condition can the approach lightsystem serve as a necessary visual reference for descent below DHor 1To the manager of the General Aviation District MDA. Office. 2To the manager of the facility in control at the timeof 2Descent to the intended runway is authorizedas long as the deviation. any portion of the approach light system can beseen. 3Upon request by ATC, submit a written report to the ATC 3The approach light system can be usedas a visual manager. reference, except that descent below 100 feetabove TDZE requires that the r id light bars bevisible and 5079. A pilot approaching to land a turbine-powered aircraft identifiable. on a runway served by a VASI shall

5072. What altitude is a pilot authorized to flywhen cleared 1not use the VASI unless a clearance fora VASI for an ILS approach? The pilot approach is received. 2use the VASI only when weather conditions are below 1may begin a descent to the procedureturn altitude. basic VFR. 2must maintain the last assigned altitude until established 3maintain an altitude at or above the glide slope untila on a published route or segment of the approachwith lower altitude is necessary for a safe landing. published altitudes. 3may descend from the assignedaltitude only when 5080. Which checks and inspections of flight instrumentsor established on the final appruachcourse. instrument systems mt.st be accomplishad before an aircraft can be flown under IFR? 5078. While flying FR in controlled uirspace,if one of the two VOR receivers fails, whichcourse of action should the 1VOR within 30 days and altimeter systems and transpon- pilot in command follow? der within 24 calendar months. 2ELT testwithin 30 days, altimeter systems within 1No call Is required if one of the two VOR receivers is 12 calendar months, and transponder within 24 calendar Meriting ProPerlY. months. 2Advise ATC immediately. 3Airspeed indicator within 24 calendar months, altimeter 3 Notify the dispatcher via company frequency. system within 24 calendar months, and transponder within 12 calendar months. 5074. While flying in contro;:ad airspace,the ADF fails. What action is required? 5081. Which entryshall be recorded by the person 1Descend below positive control airspace. performing a VOR operational check? 2Advise dispatch via company frequency. 1Frequency, radial and facility used, and bearing 3Notify ATC immediately. error. 2Right hours and number of days since last check, and bearing error. 5075. When may ATC requesta detailed report on an emergency even though a rule has not been violated? 3Date, place, bearing error, and signature. 1When priority has been given. 5082. What is the maximum permissible variation between 2Anytime an emergency occurs. the two bearing indicators on a dual VOR systemwhen checking one VOR against the other? 3--When the emergency occurs in controlledairspace. 1-4. on the ground and in flight 2f on the ground and in flight 3-8' in flight and r on the ground.

616 50113. What record shall be made by the pilot performing a 5059. Which of the following is a transponder requirement VOR operational check? for helicopter operations? 1The date, frequency of VOR or VOT, number of hours 1Helicopters with a certified cross weight of more than flown since last check, and signature in the aircraft log. 12,500 pounds that are ,ngaged in commercial oper- 2The date, place, bearing error, and signature in the ations are required to bo equipped with operable ATC aircraft log or other record. transponders. 3The date, approval or disapproval, tech reading, and 2Under the terms of a letter of agreement, helicopters signature in the aircraft log or other permanent record. may be operated at or below 1,000 feet AGL within TCA's without an operable ATC transponder. 5094. During a VOT check of the VOR equipment, the 3Operable ATC transponders are required when opera'Jng coursedeviationindicatorcenters on 356'withthe helicopters within control zones at night under special TO/FROM reading FROM. This VOR equipment may VFR.

1be used If 4' is entered on a correction card and 5090. In addition to a two-way radio capable of communi- subtracted from all VOR courses. cating with ATC on appropriate frequencies, which equip- 2be used during IFR flights, since the error is within limits. ment Is the helicopter required to have to operate within a 3not be used during 1FR flights, since the TO/FROM Terminal Control Area? (Letter of agreement not applicable.) should read TO. 1A VOR or TACAN receiver. 50115. If an airborne checkpoint is used to check the VOR 2DME, a VOR or TACAN receiver, and an appropriate system for IFR operations, the maximum bearing error transponder beacon. permissible is 3An appropriate radar beacon transponder. 1plus or minus 6'. 5091. In addition to the localizer,glide slope, marker 2plus 6' or minus V. beacons, approachlighting,and HIRL, which ground 3plus or minus 4'. components are rcquired to be operative for a Category II instrument approach to a DH below 150 feet AGL? 50011. A function of the minimum equipment listis to indicate required items which 1RCLS and REIL 2Radar and RVR. 1are required to be operative for overwater passenger air 3TDZL, RCLS, and RVR. wrier flights. 2may be inoperative for a one-time ferry flight of a large 5092. When may a pilot descend below 100 feet above the airplane to a maintenance base. touchdown zone elevation during a Category II ILS instru- 3may be inoperative prior to beginning a flight in a ment approach when only the approach lights are visible? muldengine airplane. 1After passing the visual descent point (VDP). 5057. When is DME required for an instrument flight? 2When the RVR is 1,600 feet or more. 3When the red terminal bar of the approach light systems 1At or above 24,000 feet MSL if VOR navigational are in sight equipment is required. 2In terminal radar service areas. 5093. Which ground components arerequiredto be 3Above 12,500 feet MSL operative for a Category II approach in addition to LOC, glide slope, marker beacons, and approach lights? 505$. In what altitude structure Is a transponder required when operating in controlled airspace? 1Radar and RVR. 2RCLS and REIL 1Above 12,500 feet AGL, excluding the airspace at and 3HIRL, TD2L, RCLS, and RVR. below 2,500 feet AGL 2Above 12,500 feet MSL, excluding the airspace at and 5094. Information obtained from flight data and cockpit below 2,500 fest AGL voice recorders shall be used only for 3Above 14,600 feet MSL, excluding the airspace at and below 2,500 feet AGL 1determining who was responsible for any accident or incident. 2determining evidence for use in civil penalty or certificate action. 3determining possible causes of accidents or incidents.

7 17 1 5095. For what purpose may cockpit voice recorders and 5101. Which operational requirement must be observed by flight data recorders not be used? a commercial operator when ferrying a large, three-engine, turbojet-powered airplane from one facility to another to 1Determining causes of accidents and occurrences under repair an inoperative engine? kwestigation by the NTSB. 2Determining any certificate action, or civil penalty, arising 1The computed takeoff distance to reach V1 must not out of an accident or occurrence. exceed 70 percentof the effective runway length. 3--Identifying procedures that may have been conducive to 2The existingandforecastweather fordeparture, any accident, or occurrence resulting in investigation en route, and approach must be VFR. under NTSB Part 830. 3No passengers can be carried.

5008. How long Is cockpit voice recorder and flight recorder 5102. A person may not act as a crewmember of a civil data kept, in the event of an accident oroccurrence aircraft if alcoholic beverages have been consumed by that resulting in terminating the flight? person within the preceding 1-40 days. 1-8 hours. 2-90 days. 2-12 hours. 3-30 days. 3-24 hours.

1097. A commercial operator plans to ferry a large, four- 5103. How may an aircraft operate in North Atlantic (NAT) engine, reciprocating-engine-powered airplane fromone Minimum Navigation Performance Specifications Airspace facility to another to repair an inoperative engine. Which is with less than the minimum navigation capability required by an operational requirement for the three-engine flight? FAR Part 91, appendix C? By 1The gross weight at takeoff may not exceed 75 percent 1operating under VFR conditions only. of the mend um certificated gross weight 2requesting a deviation from the Administrator. 2Weather conditions at the takeoff and destination 3operating only between 2400Z and 0800Z. airports must be VFR. 3The computed takeoff distance to reach V1 must not 5104. Which publication includes information on operatinns exceed 70 percent of the effective runway length. in the North Atlantic (NAT) Minimum Navigation Perform- ance Specifications Airspace? 1008. Which operational requirement must be observed when ferrying an air carrier airplane when one of its three 1FAR Part 121. turbine engines is Inoperative? 2ICAO Annex 1, Chapter 2. 3FAR Part 91. 1The weather conditions at takeoff and destination must be VFR. 5105. When a certificate holder is notified that a person 2The flight cannot be conducted between officialsunset specifically authorized to carry a deadly weapon is to be and official sunrise. aboard an aircraft (except in an emergency), how long 3Weather conditions must exceed the basic VFR mini- before loading that flight should the air carrier be notified? mums for the entire route, including takeoff and landing. 1-5 hours. 5099. Which operational requirement must be observed 2-2 hours. when ferrying a large, turbine-engine-powered airplane when 3-1 hour. one of its engines is inoperative? 5108. When a person, in the custody of law enforcement 1The weather conditions at takeoff and destinationmust personnel, is scheduled on a flight, what procedures are be VFR. required regarding boarding of this person and the escort? 2Weather conditions must exceed the basic VFRmini - mums for the entire route, including takeoff and landing. 1They shall enplane and depart before all other passen- 3The flight cannot be conducted between official sunset ger and sunrise. 2They shall be boardedafterallother passengers enplane, and deplaned before allother passengers 5100. When a turbine-engine-powered airplane is to be deplane. ferried to another base for repair of an inoperative engine, 3They shall be boarded before allother passengers which operational requirement must be observed. enplane, and deplaned after all passengers have left the aircraft 1Only the required flight crewmembers may beon board the airplane. 2The odsting and forecast weatherfordeparture, en route, and approach must be VFR. 3No passengers except authorized maintenanceperson- nel can be carried.

18 .8 must be the 5107. When a passenger notifies the certificate holder prior 5113. What restrictions observed regarding of In the ment of an to cheoldng baggage that an unloaded weapon is in the carrying cargo passenger compart FAR Pert 121? baggage, what action is required by regulation regarding this airplane operated under *OW? 1All cargo must be separated from all seated passengers a of certain load 1The baggage may be carried In the flightcrew compart- by partition capable withstanding ment, provided the baggage remains locked stresses. 2The *gage must remain locked and only the passen- 2Cargo may be carried aft of a divider if properly secured ger retains the ksy. by a safety belt be In a bin end secured The baggage must remain locked and custody of the key 3All cargo must carded suitable shelf remain with a designated person other than the to the floor structure of the airplane. owner of the weapon. 5114. What requirement must be met regarding cargo that of an air 5110t Which applies to the carriage of a person in the is carded anywhere in the passenger compartment custody of law enforcement personnel? carder airplane. 1The air carrier is not allowed to serve a meal to the 1The bin In which the cargo is carded may not be or use of, person in custody. installed in a position that restricts access to, 2No more than one person In custody may be carried on any emergency exit in the rear of the a flight if the person le considered to be in a maximum 2Cargo may not be carried anywhere risk category. passenger compartment. In the is carried must 3The person in custody and the escort must remain 3The container or bin which cargo seated for the entire fight be made of material which is at least flash resistant a 5100. With whom must the crew of a domestic and flag air 5115. Information recorded during normal operation by in a carder airplane be able to communicate, under normal required cockpit voice recorder passenger-carrying condition% along the entire route of flight airplane 1Any FSS. 1must be retained for 30 minutes after landing. 2ARINC 2may be erased only once each flight 3Company dispatch office. 3may all be erased except the last 30 minutes. 5110. With whom must the crew of a domestic and flag air 5116. Which rule applies to the use of the cockpit voice carrier airplane be able to communicate, under normal recorder erasure feature? conditions, along tit, entire route of flight? 1All recorded information may be erased at the end of a 1Any FS& flight 2ARINC 2Any Information more than 30 minutes old may be 3Air Traffic Control. erased 3Any ground operation that was recorded may be erased. 5111. For which of these aircraft is the "clearway" for a the of the recorder system, particular rurnvay considered In computing takeoff weight 5117. For p...pose testing flight Nmitations? 1a maximum of 45 minutes of the oldest prerecorded data aircraft may be erased. 1--Passenger-carrying transport 2U.S. certified air carder airplanes. 2a total of 1 hour of the oldest recorded data accumulated at the time of may be erased. 3Turbine-engine-powered transport airplanes. testing 3--a total of no more than 1 hour of recorded data may be 5112. What effective runway length is required for a erased airplane at the destination airport if the turbojet-wavered be runways are forecast to be wet or slippery at the ETA? 5110. When must a cockpit voice recorder operated? to 1-70 percent of the actual runway available. 1From the start of the before starting engine checklist 2-150 percent of the runway length required for a dry completion of checklist prior to engine shutdown. 2From the start of the before startng engine checklist to runway. of 9-115 percent of the runway length required for a dry completion of final checklist upon termination flight. taxi for to shutdown runway. 3When starting to takeoff engine after termination of flight

919 5119. If there is a required emergency exit located in the 5127. If an air carrier airplane's airborne radar is inoperative flightcrew compartment, the door which separates the and thunderstorms are forecast along the proposed route of compartment from the passenger cabin must flight, an airplane may be dispatched only 1be locked at all times, except during emergencies, while 1when two alternate airports are filed. lancing. 2If the flight is filed IFR. 2be locked at all times, except during any emergency 3In day VFR conditions. declared by the pilot in command. 3be latched open during takeoff and landing. 5128. If an air carrier airplane is flying IFR using single ADF navigation receiver and the ADF equipment falls, the 5120. If a passenger-carrying landplane is required to have flight must be able to an automatic deploying escape slide system, when must this system be armed? 1proceed safely to a suitable airport using VOR aids and complete an Instrument approach. 1During taxi, takeoff, and landing. 2continue to the destination airport by means of dead 2Only for takeoff and lauding. reckoning navigation. 3Only for taxi and takeoff. 3 proceed to and land at a flied en route alternate airport.

5121. If a turbine-engine-powered, pressurized airplane is 5129. What action should be taken by the pilot in command not equipped with quick-donning oxygen masks, what is the of a transport category airplane If the airborne weather radar maximum flight attitude authorized without one pilot wearing becomes inoperative en route on Pn IFR flight for which and using an oxygen mask? weather reports Indicate possible thunderstorms? 1FL300. 1Request radar vectors from ATC to the nearest airport 2FL250. suitable for large aircraft landings. 3FL200. 2Proceed In accordance with the approved instructions in the operations manual. 5122. If either pilot of an air carrier airplane leaves the duty 3Return to the departureairportifcloser than the station while flying at FL310, the other pilot destination airport 1shall put on and use an oxygen mask 5130. When a pilot plans a flight using NDB NAVAIDS, 2must have a quick-donning type oxygen mask available. which rule applies? 3and the flight engineer shall put on and use their oxygen mask 1An alternate airport must be filed that has a radar approach available. 5123. Which airplanes are required to be equipped witha 2The pilot must be able to return to the departure airport ground proximity warning glide slope deviationalerting using other navigation radios. system? 3The airplane must have sufficient fuel to proceed, by 1--AN turbojet-powered airplanes. means of VOR NAVAIDS, to a suitable airport and land. 2Passenger-carrying airplanes only. 5131. When must an air carrier airplane be DME equipped? 3Large turbine-powered airplanes only. 1Whenever VOR navigationalreceivers arerequired. 5124. When may two persons share one seatbelt ina 2For flights at or ebove 18,000 feet MSL lounge seat? 3In the Continental Control Area for all IFR or VFR On Top operations. 1When one is an adult and one is a child under 3years of age. 5132. When an air carrier flight is operated under IFR or 2Only during the en route portion of a flight over-the-top on "victor airways," which navigation equip- 3During all operations except the landirj portion of a ment is required to be installed in duplicate? SOK 1ADF. 5125. While on an IFR flight in controlled airspace, the 2VOR. failure of which unit will precipitate an Immediate report to 3Marker beacon receiver. ATC? 5133. The emergency lights on a passenger-carrying air- 1--Seocnd ary or backup attitude indicator. 2Airborne radar altimeter. plane must be armed or turned on during 3DME. 1preflight prior to night operations. 2taxiing, takeoff, and landing. 5128. An air carrier airplane's airborne radar must be in 3preflight prior to every flight satisfactory operating condition prior to dispatch, If the flight will be 1conducted under IFR conditions and thunderstorms are reported in route. 2 carryingpassengers,butnotIfitIs"ailcargo." 3 conducted over water more than 50 miles from shore.

1020 5134. Federal Aviation Regulations require that interior 5140. What emergency equipment i3 required for extended emergency Nghts must overwater operations? 1operate automatically when subjected to a negative 1A portable emergency radio transmitter for each crew- CI load. member. 2be operable manually from the fiightcrew station and the 2A survival kit for each life preserver. passenger compartment. 3A life preserver equipped with a survivor locator light, for 3be armed 6 turned on during ground operation and all each occupant. flightof 5141. Each large aircraft operating over water must have a 5135. Where should the portable battery-powered mega- life preserver for each phone be located if only one is required on a passenger- carrying airplane? 1seat on the aircraft. 2occupant. 1The most rearward location in the passenger cabin. 3seat, plus 10 percent 2The most forward locationin the passenger cabin. 3In the passenger cabin near the overwing emergency 5142. For a flight over uninhabited terrain, an airplane exit operated by a flag or supplemental air carrier must carry enough appropriately equipped survival kits for 5136. How many portable battery-powered megaphones are required on an air carrier airplane with a seating 1-50 percent of the passengers. capacity of 100 passengers on a tripsegment when 2all occupants of the airplane. 45 passengers are carded? 3all paying passengers. 1Two; one at the forward end and the other at the most 5143. When a supplemental air carrier is operating over an rearward location in the passenger cabin. uninhabited area, how many appropriately equipped survival 2One; at the most rearward location in the passenger kits are required aboard the airplane? cabin. 1One for each passenger seat 3Two; one located near or accessible to the flightcrew 2One for each four passengers. and me located near the center of the passenger cabin. 3Enough for the number of occupants of the airplane.

5137. How many portable battery -powered megaphones 5144. Life preservers required for overwater operations are are required on an aircarrier airplane with a seating stored capacity of 150 passengers on a trip segment when 75 passengers are carried? 1adjacent to every emergency exit. 2behind the cockpit bulkhead. 1Two; one located near or accessible to the flightcrew, 3within easy access in the event of ditching. and one located near the center of the passenger cabin. 2One; at the most rearward location in the passenger 5145. An airplane operated by a supplemental air carrier cabin. flying over uninhabited terrain must carry which emergency 3Two; one et the forward end, and the other at the most equipment? rearward location of the passenger cabin. 1Survival saw. 51311. In the event of an engine emergency, the use of a 2Pyrotechnic signaling device. cockpit check procedure by the flightcrew is 3Colored smoke flares.

1discouraged because of possible failure of the cockpit 5146. An airplane operated by a commercial operator flying lighting system. over uninhabitedterrainmust carry which emergency 2required by regulations to prevent reliance upon memo- equipment? rized procedures. 3--recomrnendad by the FM as a doublecheck after the 1Colored smoke flares. memorized procedure has been followed. 2Pyrotechnic signaling device. 3Survival saw. 5139. Which emergency equipment is required for a flag air Mier flight between John F. Kennedy International Airport 5147. An airplane operated by a flag air carrier operator and London, England? flying over uninhabited terrain must carry which emergency equipment? 1A Nfe preserver or other flotation device for the full seating capacity of the airplane. 1Pyrotechnic signaling device. 2An appropriately equipped survival kit attached to each 2Colored smoke flares. required Nferaft. 3Survival saw. 9A self-buoyant, water resistant, portable radio for each required Wendt.

(s: 1121 5140. An air carrier airplane must have an operating public 5155. What is the highest flight level that operations may address system if It be conducted without the pilot at the controls wearing and using an oxygen mask while the other pilot is away from the 1has 15 or more passengers aboard. duty station? 2has a seating capacity for more than19 passengers. 3weighs more than 12,500 pounds. 1FL410. 2FL310. 5149. A crewmember interphone systemIs required on 3FL250. which airplane? 1A large airplane. 5156. Above which cabin altitude must oxygen be provided for all passengers during the entire flight? 2An airplane with more than 19 passenger seats. 3A turbojet airplane. 1-15,000 feet 2-12,000 feet 5150. Which requirement applies to emergency equipment 3-14,000 feet. (fire extinguishers, megaphones, first aid kits, and crash ax) installed in an air carrier airplane? 5157. For a 2-hour flightin a turbine-engine-powered airplane at a cabin pressure altitude of 12,000 feet, how 1-- Cannot be located on the flight deck, all must be located In the passenger compartment much supplemental oxygen for sustenance must be provided? Enough oxygen for 2Cannot be located in a compartment or area where it is not immediately visible to a flight attendantin the 1-10 percent of the passengers for 1.5 hours. passenger compartment 2each passenger during the entire flight 3Must be dearly marked toindicateits method of 3each passenger for 30 minutes. operation. 5156. A flight crewmember must be able to don and use a 6151. Which factor determines the minimum number of quick-donning oxygen mask within hand fireextinguishersrequiredforflightunder FAR Part 121? 1-5 seconds. 2-15 seconds. 1Number of passengers aboard. 3-20 seconds. 2Number of required crewmembers. 3Number of passenger seats in the airplane. 5159. Each air carrier flight deck crewmember on flight deck duty must be provided with an oxygen mask that can 5152. Whichrestrictionappliesto a cargo binina be rapidly placed on his face when operating at flight passenger compartment? The bin altitudes above 1may have an open top if the cargo is secured bya cargo 1FL200. net 2FL250. 2must withstand the load factor required of passenger 3FL120. seats, multiplied by 1.15. 3must be equipped with an approved fire- extinguishing 5160. The supplemental oxygen requirements for passen- system and constructed of flame retardant material. gers when a flightis operated at or below FL250 is dependent upon the airplane's ability to make an emergency 5153. What is the passenger oxygen supply requirement for descent to a flight altitude of a flightwith a cabin pressurealtitudeinexcess of 15,000 feet? Enough oxygen for 1-10,000 feet within 4 minutes. 2-12,000 feet within 4 minutes or at a minimum rate of 1all passengersfor the entireflightduration above 2,500 feet per minute, whichever is quicker. 15,000 feet cabin altitude. 3-14,000 feet within 4 minutes. 2-50 percent of the actual passenger load for 30 minutes. 3-10 percent of the seating capacity at those altitudes. 5161. A passenger briefing by a crewmember shall be given, instructing passengers on the necessity and use of 5154. How much supplemental oxygen must pressurized air oxygen in the event of cabin depressurization prior to flights transport airplanes carry for each flight crewmember on conducted above flight deck duty when operating atflightaltitudes of 10,000 feet? 1FL250. 2FL240. 1A minimum of 2-hours' supply. 3FL200. 2Sufficient for the duration of the flight above 8,000 feet cabin pressure altitude. 5162. What is the minimum number of acceptable oxygen- 3Sufficient for the duration of the flight above 10,000 feet dispensing units for first aid treatment of occupants who flight altitude. might require undiluted oxygen for physiological reasons? 1Four. 2Three. 3Two.

12 2 5168. Routes that require a flight navigator are listed in the 5171. If a turbojet air carrier flight is to be operated in VFR 1 Airplane Right Manual. over-the-top conditions, which radio navigation equipment Is required to be a dual installation? 2International Flight Information Manual. 3Air Canter's Operations Specifications. 1VOR and ILS. 2VOR. 5164. Where Is a Net maintained for routes that remuire 3VOR and DME. special navigation equipment? 5172. Which equipment requirement must be met by an air 1Air Carrier's Operations Specifications. carrier that uses an Inertial Navigation System (INS) on a 2International Flight information Manual. proposed flight? 3Airplane Flight Manual. 1Dual ILS systems with an operative Flight Director 5166. WNch document includes descriptions of required System can be substituted for one inoperative INS. crew/member functions to be performed in the event of an 2A dual VORTAC/ILS system may be substituted for an emergency? Inoperative INS. 1 Airplane Flight Manual. 3Only one INS Is required if an operative Doppler Radar 2Ceracate holder's manual. can be substituted for the other INS. 3Emergency Procedures Handbook. 5173. When an air carrier airplane with a seating capacity 5166. A flight nrIgator or a specialized means of naviga- of 187 has 151 passengers on board, what is the minimum tion Is required aboard an air carrier airplane operated number of flight attendants required? outside the 48 contiguous states and District of Columbia 1Five. when 2Four. 1the airplane's position cannot be reliably fixed for a 3Three. period of more than 1 hour. 5174. An airplane has a seating capacity of 149 passen- 2operations are conducted IFR or VFR On Top. gers. What Is the minimum number of flight attendants 3operations are conducted over water more than 50 miles required with 97 passengers aboard from shore. 1Four. 5167. Required crewmember functions to be performed In 2Three. the event of an emergency shall be assigned by the 3Two. 1pilot in command. 5175. The "age 80 rule" of FAR Part 121 applies to 2ak carrier's chief pilot 3certillcate holder. 1any required pilot crewmember. 2any pilot or flight engineer. 5168. What is the minimum number of flight attendants 3the pilot in command only. required for an airplane having a seating capacity of 178 passengers with only 113 passengers aboard. 5176. When the need for a flight engineer Is determined by 1 Flue. aircraft weight, what is the takeoff weight above which a 2Four. flight engineer Is required? 3Three. 1-80,000 pounds. 2-12,500 pounds. 5180. What is the minimum number of flight attendants 3-300,000 pounds. required for an air carrier airplane with a seating capacity for 335 passengers when 299 passengers are aboard? 5177. Under which condition is a flight engineer required as 1Seven. a flight crewmember in FAR Part 121 operations? 2Six. 1If the airplane has a seating capacity for 30 passengers 3 Five. or more. 2If the airplane is powered by more than two engines. 5170. An air carrier that elects to use an Inertial Naviga- 3If required by the airplane's type certificate. tional System (INS) must meet which equipment requirement prior to takeoff on a proposed flight? 5178. If a flight engineer becomes incapacitated during flight, who may perform theflightengineer's duties? 1One INS with a dual VORTAC/ILS system may be used as a baciwp. 1The second In command only. 2Dual ILS systems with an operative Flight Director 2Any crewmember designated by the pilot in command. System may be used as a backup for one inoperative 3Either pilot,ifqualifiedto performflightengineer INS. functions. 3One INS may be Inoperative, but an operational Doppler Radar unit may be substituted in ho stead.

It 3 5179. On an aircarrier airplane thatiscertifiedfor 5110. The air carrier must give instruction on such subjects operation with a flightcrew of two pilots andone flight as respiration, hypoxia, and decompression to each crew- engineer, in case of emergency, member serving on pressurized airplanes operated above 1at least one pilot must be qualified to perform flight 1-20,000 feet. engineer duties. 2-12,000 feet. 2the flight engineer must be qualified to perform duties at 3-25,000 feet. one pilot position. 3each pilot must be qualified to perform flight engineer 5137. A pilot in command must complete either a profi- duties. ciency check or simulator training within the preceding

51110. When a flight engineer is a required crewmemberon 1-6 months. a flight, it Is necessary for 2-12 months. 3-24 months. 1at least one pilot to hold a Flight Engineer Certificate. 2the flightengineer to be properly certificated and 5111. Any person whose duties include the handling or qualified, but there is no requirement for any other carriage of dangerous articles and c nagnetized materials crewmember to be qualified or certified to perform flight must have satisfactorily completed an establit hed and engineer duties. approved training program within the preceding 3at least one pilot to be qualified to perform flight 1-24 calendar months. engineerduties,but a certificateisnot required. 2-12 calendar months. 5151. If a flight crewmember completes a required annual 3-6 calendar months. flight check in December 1987 and the required annual 5189. A pilot recurrent flight check in January 1989, the latter check is flight crewmember, other thanpilotin considered to have been taken in command, must have received either a proficiency check or line-oriented simulator training within the preceding IDecember. 2January 1-6 months. 3November. 2-12 months. 3-24 months. 5182. What is the term for the training required for flight crewmembers who have not qualified and served in the 5190. Which is one of the requirements that must be met same capacity on another airplane of the same group by a required pilot flight crewmember in re-establishing (e.g., turbojet powered)? recency of experience? 1Upgrade training. 1At least one landing must be made to a full stop with a 2Primary training. simulated failure of the most critical engine. 3Initial training. 2At least one landing must be made from an ILS approach to the lowest ILS minimums authorized for the 5183. A crewmember who has servedas second in certificate holder. command on a particular type airplane (e.g., B-727-100), 3At least two landings must be made to a complete stop. may serve as pilot in command upon completing which Paining program? 5191. What is one of the requirements that must be met by an airlinepilot to re-establish recency of experience? 1Upgrade training. 2Recurrent training. 1At least one landing approach must be made from a 3Initial training. circling instrument approach. 2At least one landing must be made to a full stop. 5184. What is the term for the trainingrequired for 3At least one nonprecislon approach must be made to the asvernembers or dispatchers who have qualified and served lowest minimums authorized for the certificate holder. in the same capacity on other airplanes of thesame group? 5192. What are the line check requirements for the pilot in 1Difference training. command for a domestic air carrier? 2Transition training. 3Upgrade training. 1The line check isrequired only when the pilotis scheduled to fly a new route. 51$5. How often must a crewmember actually operate the 2The line check is required each 12 calendar months in airplane emergency equipment? Once every one of the types of airplanes to be flown. 3The line check is required each 12 months in each type 1-8 calendar months. aircraft in which the pilot may serve. 2-12 calendar months. 3-24 calendar months. 5193. Normally, a dispatcher should be scheduled for no more than

1-8 consecutive hours ofserviceinany 24 hours. 2-8 hours of serviceinany 24 consecutive hours. 3-10 hours of service inany 24 consecutive hours. 14 24 1184. An aircraft dispatcher shall receive at least 24 con- 5201. A flag air carrier may schedule a pilot of any airplane, *Boutin hours of rest during each having two pilots and one additional crewmember, for no more than 1-120 consecutive hours. 2-7 consecutive days. 1-8 hours during any 12 consecutive hours. 9-10 consecutive days. 2-10 hours during any 12 consecutive hours. 3-12 hours during any 24 consecutive hours. 5185. To remain current as an aircraft dispatcher, a person must, in addition to other requirements, 5202. What is the maximum flight time in 24 consecutive Flu irs that a flag air carrier may schedule a pilot in a two- 1make a trip over one of the air carrier's routes within the pilot crew without a rest period? preoeffing 8 calendar months. 2spend 5 hours observing flight deck operations within the 1-8 hours. preceding 12 calendar months. 2-10 hours. 3make a trip in one of the types of airplanes to be 3-12 hours. &patched, every 3 calendar months. 5203. What is the maximum number of hours a pilot may fly 5188. Ifa domestic or flagaircarrier schedules a in 7 consecutive days as a pilot in a two-pilot crew for a flag dlepatcher for 13 hours of duty in a 24-consecutive-hour air carder? period, what action is required? 1-35 hours. 1The dispatcher should report a violation of FAR Part 121 2-32 hours. to the air carrier's director of operations. 3-30 hours. 2Within 72 hours, the dispatcher should report a violation of FAR Part 121 to the supervising air carrier district 5204. What isthe maximum number of hours that a office. supplemental air carder pilot may fly in 30 consecutive 3The dispatcher should be given a rest period of at least days? 8 hourat or before the completion of 10 hours of duty. 1-100 hours. 5187. Duty and rest period rules for domestic air carrier 2-120 hours. operations require that a flight aewmember 3-300 hours. 1not be assigned to any duty with the air carrier during a 5205. How many hours may a supplemental air carrier pilot requked rest period. on a three-pilot crew be scheduled for flight deck duty 2not be on duty aloft for more than 90 hours in any during any 24-hour period? calendar month. 3be relieved of all duty for at least 48 hours during any 1-8 hours. 7 consecutive days. 2-8 hours. 3-10 hours. 5199. When a flag air carrier airplane re.7.4res more than one flight engineer or flight navigator, which flight time 5208. Theflighttimelimitationsestablishedforflight aewmembers include limitation applies during any 12 calendar months? 1-1,000 hours. 1all commercial flying in any flight crewmember position. 2-1,100 hours. 2only commercial flying in any flight crewmember position 2-1,200 hours. inwhich FAR Part 121operations are conducted. 3allflighttimeinanyflight crewmember position. 5109. What is the maximum number of hours that a pilot may fly as a crewmember in domestic air carrier service? 5207. Which passenger announcement must be made after each takeoff? 1-120 hours in any 30 consecutive days and 1,200 hours in any 12 consecutive months. 1The location and use of emergency exits. 2Keep seatbelts fastened while seated. 2-120 hours in any calendar month and 1,000 hours in any calendar year. 3How to use the passenger oxygen systemin an emergency. 3-100 hours in any calendar month and 1,000 hours in any calendar year. 5208. What information must the pilot in command of a domestic air carder flight carry to the destination airport? $200. How does deadhead transportation atfect the computation of flight time limits for air carrier flight crewmembers? ICargo and passenger distribution Information. It is 2Copy of the flight plan. 1considered pert of the rest period if the flightcrew 3Names of all crewmembers and designated pilot in command. includes more than two pilots. 2not considered part of the rest period. 3considered part of the rest period for flight engineers and navigators.

5 5209. How long may a domestic air carrier flight remain on 5217. When the pilotin command Is responsible for a the ground at an intermediate airport before fispatch deviation during an emergency, the pilot should submit a release is required? written report within 1-1 hour. 1-48 hours after the deviation. 2-2 hours. 2-24 hours after returning to home base. 3-6 hours. 3-10 days after returning to home base.

5210. When an intoxicated person creates a disturbance 5218. What action should the pilot in command follow If it is aboard an air carder aircraft, within what period of time must necessary to shut down one of the two engines on an air the certificate holder submit a written report, concerning the carrier airplane? incident, to the Administrator? 1Land at any airport the pilot considers as safe as the 1-7 days. nearest suitable airport in point of time. 2-5 days. 2Proceed to the airportspecifiedby the company 3-48 hours. dispatcher. 3Land at the nearest suitable airport in point of time at 5211. Which applies when carrying a passenger aboard an which a safe landing can be made. all-cargo aircraft? 5219. Assuring that appropriate aeronautical charts we 1The passenger must have a seat reserved on the flight aboard an aircraft is the responsibility of the deck. 2The pilot in command may authorize the passenger to 1eircref t dispatcher. be admitted to the crew compartment 2flight navigator. 3Crew-type oxygen must be provided for the passenger, 3pilot in command.

5212. Each crewmember shall have available for individual 5220. Which persons are jointly responsible for the Initi- use on each flight a ation, continuation, diversion, and termination of a supplemental air carrier or commercial operator flight? 1pyrotechnic signaling device. 2hand fire extinguisher suitable for combating Class A, B, 1 Pilot in command and aircraft dispatcher. and C fires. 2Director of operations and chief pilot 3flashlight in good working order. 3Pilot In command and director of operations.

5213. Following the stoppage of an engine's rotation in 5221. The pilot in command has emergency authority to flight, the pilot in command must, as soon as practicable, exclude any and all persons from admittance to the flight first report the occurrence to the deck 1- -appropriate ground radio station. 1with the exception of any certified FAA inspector. Pnearest air carder district office. 2as an emergency action in the interest of safety. 6operations manager (or director of operations). 3except those persons who have specific authorization of the certificate holder and the FAA. 5214. Should it become necessary to shut one engine down on a domesticaircarrierthree-engine turbojet 5222. If an aircraft dispatcher cannot communicate with an airplane, the pilot in command air carrier flight during an emergency the aircraft dispatcher should 1may continue to the planned destination if approved by the company aircraft dispatcher. 1take any action considered necessary under the circum- 2may continue to the planned destinationIfthisIs stances. considered as safe as landing at a closer airport. 2comply with the company's lost aircraft plan. 3must land at the nearest airport that a landing can be 3notify transit alert. mode. 5223. Who is required to submit a written report on a 5215. What is the maximum number of continuous hours of deviation that occurs during an emergency? duty that anaircraftdispatcher may be scheduled? 1Pilot in command. 1-8 hours. 2Dispatcher. 2-10 hours. 3Person who declares the emergency. 9-12 hours.

5216. When an aircraft dispatcher declares an emergency for a flight and a deviation results, a written report shall be sent to the 1ATC facility chief within 48 hours. 2nearest FM district office within 48 hours. 3FM Administrator within 10 days. 26 18 II124. When a departure alternate is required for a three- 5230. Which inflight conditions are required by a supple- engine air Mier flight, it must be located at a distance not mental air carrier to conduct a day, over-the-top flight below peaty than the specified IFR minimum en route altitude? 1-2 hours from the departure airport at normal cruising 1The flight must remain clear of clouds by at least speed In et' air with one engine inoperative. 500 feet vertically and 1,000 feet horizontally and have 2-1 hour from the departure airport at normal cruising at least 3 miles flight visibility. speed in still air with one engine inoperative. 2The flight must be conducted at least 1,000 feet above 9-2 hours from the departure airport at r -..,mal cruising an overcast or broken cloud layer and have at least speed in still air. 5 miles flight visibility. 3The height of any higher overcast or broken layer must 5225. When is a supplemental air carrier, operating under he at least 500 feet above the IFR MEA. FR. required to Net an alternate airport for each destination airport within the 48 contiguous United States? 5231. Prior to listing an airport as an alternate airport in the dispatch or flight release, :weather reports and forecasts 1When the forecast weather indicates the ceiling will be must indicate that weather conditions at that airport will be lees than 2,000 feet and visibility less than 3 miles at at or above authorized minimums the estimated time of arrival. 2An alternate airport is required regardless of existing or 1for a period 2 hours before and 2 hours after the ETA. forecast weather condition. 2during the entire flight 3When the flight is scheduled for more than 6 hours 3when the flight arrives. en route. 5232. What minimum weather conditions must exist for an sue. If a four-engine air carrier airplane is dispatched from airport to be listed as an alternate in the dispatch release an airport that is below landing minimums, what is the for t. domestic air carrier flight? Those maximum distance that a deperare alternate airport may be located from the departure airport? 1listed on the NOAA IAP chart for the alternate airport, at the time the flight is expected to arrive. 1Not more than 1 hour of normal cruise speed In still air 2specified in the certificate holder's operations specifica- with one engine inoperative. tions for that airport, when the flight arrives. 2Not more than 2 hours at slow cruliie speed in still air 3listed on the NOAA IAP chart for the alternate airport, with one engine inoperative. from 2 hours before to 2 hours after the ETA for that 3Not more than 2 hours at normal cruise speed in still air flight with one engine inoperative. 5233. Which dispatch requirement applies to a flag air 1227. Whatisthe maximum distance requiredfor a carrier scheduled for a 7-hour IFR flight? departure alternate airport for two-engine airplanes? 1No alternate airport is required if the forecast weather at 1-1 hour at normal cruise speed in still air with one engine the ETA at the destination airport is at least 1,E00 feet operating. and 3 mites. 2-1 hour at normal cruise speed instillair with both 2An alternate airport is required. engines operating. 3An alternate airport is required only if it is specified in the 3-2 hours at normal cruise speed instillair with one International Flight Information Manual. engine operating. 5234. An &port is not listed in a domestic air carrier's 5221. An alternate airport for the airport of takeoffis operations specifications and does not have prescribed required takeoff weather minimums. What are the minimum weather conditions for takeoff? 1If weather conditions are below authorized landing minimums. 1-1000-3. 2when no destinetionalternateairportisavailable. 2-900-2. 3when destinption weather is marginal VFF', (ceiling less 3- 800-2. than 3,000 feet and visibility less than 5 SM). 5235. The pilotin command of an airplane en cute 5229. When the forecast weather conditions for a destina- determines that icing conditions can be expected that might tion and alternate airport are considered marginal for a adversely affect safety of theflight.Which actionis domestic air carrier's operation, what specific action should appropriate? the pilot in command take? 1The pilot in command and the company dispatcher must 1Delay the flight, not to exceed 1 hour, for possible jointly decide whether or not the flight may continue to weather improvement the original destination airport 2Add 1 additional hour of fuel based on cruise power 2The pilot in command shall not continue flight into the settings for the airplane in use. icing conditions. 3Ust at least one additional alternate airport. 3The flight may continue to the original destination airport, provided all anti-icing and deicing equipment is 0Per- atonal and is used.

( 17 27 MIL What action is required prior to takeoff if snow is 5243. When a flagaircarrierairplanelandsat an adhering to the wings of en dr carrier airplane? intermediate airport at 1322Z, what is the latest time it may continue a flight without receiving a redispatch authoriza- 1. -Tum on wing deice prior to takeoff. tion? 2Assure that the snow is removed. 9Add 15 knots to the normal W Vasa 1-1922Z. 2- 1622Z. 5237. When an alternate airport outside the United States 3-1422Z. has no prescribed takeoff minimums and is not listed In a flag air carrier's operations specifications, what minimum 5244. When a flag air carrier flight lands at an intermediate weather conditions will meet the requirements for takeoff? airport at 13452id experiences a delay, what is the latest 1-800-2-1/2. time it may dep& c for the next airport without a redispatch 2-800-3. release? 3-900-1-1/2. 1-1945Z. 2 -15452 523$. What minimum weather conditions must exist for a 3- 14452. domestic air carrier flight to take off from an airport within the United States which is not listed In the air carrier's 5245. The reserve fuel supply for a domestic air carrier operationsspecifications?(Takeoff minimums arenot flight is prescribed for that airport) 1-30 minutes of holding fuel consumption 1,500 feet 1-800-2, 100-1/2, or 1500-1. above the destination or alternate airport 2-800-2, 900-1-1/2, or 1000-1. 2-45 minutes at normal fuel consumption in addition to the 3-800. 3,1000.2, or 1200-1. fuelrequired to the most distant alternateairport. 3-45 minutes of holding fuel consumption 1,500 feet 5239. An alternate airport is not required to dispatch a flag above the destination or alternate airport. sir carrier airplane for a flight less than 6 hours when the visibility for at least 1 hour before and 1 hour after the ETA 5246. What is the minimum fuel required by a flag air carrier at the destination airport is forecast to be turbojetairplane on a flightwithin the 48 contiguous 1-2 miles or greater. United States, after reaching the most distant alternate 2at least 3 miles, or 2 miles more than the lowest airport? opplicable minknum. 1-45 minutes at normal cruising fuel consumption. 3at least 5 miles. 2-2 hours at normal cruising fuel consumption. 3Enough fuel to return to the destination airport. 5240. Which weather conditions meet the minimum requirements for a flag air carrier to take off from an alternate 5247. What is the fuel reserve requirement for a commer- airport that is not listed In the operation specifications? cially operated reciprocating-engine-powered airplane flying 1-800-1/2, 900-1, 1000-2. within the contiguous United States upon arrival at the most 2-800-1, 900.2, 1000-3. distant alternate airport specified in the flight release? Enough fuel to fly 3-800-2, 900.1-1/2, 1000-1. 1-30 minutes plus 15 percent of total time required to fly at 5241. When a domestic air carrier airplane lands atan normal cruising consumption to the alternate. Intermediate airport at 1815Z, what is the latest time itmay 2-45 minutes at normal cruising fuel consumption. depart that airport without a specific authorization froman 3-15 minutes plus 30 percent of the total time required to aircraft dispatcher? fly to the alternate at normal cruising fuel consumption. 1-19451 2-1915Z. 6246. For a flag air carrier flight to be released to an island 3-18451 airport for which an alternate airport is not available, a turbojet- powered airplane must have enough fuel to fly to 5242. When a flag air carrier flight lands at an intermediate that airport and thereafter to fly airport at 1805Z, what is the latest time it may depart 1for 2 hours at normal cruisingfuelconsumption. without being redispatched? 2for 2 hours at a fuel consumption computed for 1-0005Z. 10,000 feet MSL at a specific weight and holding 2-20051 &speed 3-19051 3back to the departure airport.

28 5249. An alter nate airport is not required for a supplemental 5256. Under what conditions may an aircarrierpilot or commercial air carrier, turbojet-powered airplane on an continue an instrument approach to the DH or MDA, after IFR flight outside the 48 contiguous states, if receiving a weather report Indicating that less than minimum published landing conditions exist at the airport? 1i fuel reserve for 30 minutes, plus 15 percent of the total flight time, Is carried aboard the airplane. 1If the instrument approach is conducted in a radar 2enough fuelis aboard the airplanetoflyto the environment destination and thereafter to fly for at least 2 hours at 2When the weather report is received after the pilot has normal cruising fuel consumption. been cleared for an instrument approach. 3enough fuel to fly for 30 minutes at holding airspeed at 3Whan the weather report is received after the pilot has 1,500 feet AOL is carried aboard the airplane. begun the final approach segment of an Instrument approach. 5250. What is the fuel reserve required for a turbine-engine- powered (other than turbopropeller) supplemental air carrier 5257. By regulation, who shall provide the pilot in command airplane upon arrival over the most distant alternate airport of a domestic or flag air carrierairplane,information outside the contiguous United States? concerning irregularities of facilities and services? 1-30 minutes at holding speed. 1Air route traffic control center. 2-45 minutes at normal cruising speed. 2Director of operations. 3-2 hours at normal cruise fuel consumption. 3Aircraft dispatcher.

5251. Upon arriving at the most distant airport, what is the 5258. Who is responsible for obtaining information on all fuel resorts requirement for a turbopropeller flag air carrier current airport conditions and irregularities of navigation airplane. facilities for a supplemental air carrier flight? 1-30 minutes at the most economical altitude for fuel 1Aircraft dispatcher. consumption at holding speed. 2Director of operations. 2-45 minutes at holding altitude. 3Pilot in command. 3-30 minutes plus 15 percent of the total time required, or 90 minutes at normal cruise, whichever is less. 5259. During a supplementalair carrierflight, who is responsibleforobtaininginformation on meteorological 5252. What Is the fuel reserve required for a turbopropeller conditions? supplemental air carrier airplane upon the arrivalat a destination airport for which an alternate airport is not 1Aircraft dispatcher. spedied 2Pilot in command. 3Director of operations. 1-30 minutes at holding airspeed. 2-2 hours at normal cruising fuel consumption. 5260. Where can the pilot of a flag air carrier airplane find 3-3 hours at normal cruising fuel consumption. the latest FDC NOTAM's?

5253. When a turbine-engine-powered flag air carrier air- 1Any company dispatch facility. plane Is released to an airport which has no available 2In the standard Instrument approach procedures book. alternate, what is the required fuel reserve? 3 Airport /Facility Directory.

1-1 hour 30 minutesat maximum rangeairspeed. 5261. Who is responsible, by regulation, forbriefing a 2-2 hours at normal cruise fuel consumption. domestic or flag air carrier pilot in command on all available 3-30 minutes plus 10 percent of the total flight time. weather information?

5254. What Is the fuel reserve required for a reciprocating- 1FSS. engine-powered supplementalaircarrierairplane upon 2Aircraft dispatcher. arrival at the most distant alternate airport during a flight 3Director of operations. within the contiguous United States? 5262. C a t e g o r y I IILS operations below 1600 RVR and a 1-45 minutes at normal cruising fuel consumption. 150-foot DH may be approved after the pilot has 2-2 hours at normal cruising fuel consumption. 1successfully completed an FAA-approved CategoryII 3-3 hours at normal cruising fuel consumption. training program. 5255. Ifaninstrument on a multiengineairplaneis 2made at least six Category II approaches in actual IFR inoperative, which document dictates whether the flight may conditionswith100-foot DH withinthepreceding continue in route? 12 calendar months. 3logged 100 hoursIlight time in make and model airplane 1Amended flight/dispatch release. and three CategoryII;LS approaches in actual or 2Original dispatch release. simulated IFR conditions with 150-foot DH since the 3Certificate holder's manual. beginning of the sixth preceding month.

19 29 5263. When a pilot's fl jht time consists of 80 hours' pilot 5271. Whichdcuments are required to be carried aboard in command in a particular type airplane, how does this each domestic air carrier flight? affect the MDA, DH, or minimum visibility for the destination airport? 1Dispatch release, load manifest, and flight plan. 2Dispatch release and weight and balance release. 1Has no effect 3Load manifest and flight release. 2MDA or DH and visibility minimums are decreased by 100 feet and 1/2 mile. 5272. How longshalla supplementalaircarrieror 3MDA or DH and visibility minimums are increased by commercial operator retain a record of the load manifest, 100 feet and 1/2 mile. flight release, and flight plan?

5264. Which information must be contained in, or attached 1-1 month. to, the dispatch release for a flagaircarrierflight? 2-3 months. 3-12 months. 1Type of operation (e.g., IFR, VFR). 2Total fuel supply on board the airplane. 5273. A domestic or flag air carrier shall keep copies of the 3Passenger manifest and cargo weight. flight plans, dispatch releases, and load manifests for at least 5265. Which certificated air carrier operators must attach to, or include on, the flight release form the name of each 1-6 months. fight crewmember, flight attondant, and designated pilot in 2-3 months. command? 3-30 days. 1Supplemental and commercial. 5274. A flag air carrier flight which requires three pilots is 2Supplemental and domestic. scheduled to operate on August 5. Each of the pilots has a 3Flag and commercial. First-Class Medical Certificate dated January 28 of the same year. For this scheduled flight 5266. What information must be contained in, or attached - to, the dispatch release for a domestic air carrier flight? 1all three pilots must have new medical certificates prior to departure. 1Departure airport, immediate stops, destinations, and 2only the pilots serving as pilot in command and secor,c; alternate airr orts. in command must have new medical certificates prior ic, 2Names of all passengers on board. departure. 3Cargo load and weight and balance data 3these medical certificates are adequate for each of the pilot positions. 5207. What information must be included on a domestic air carrier dispatch release? 5275. A certificate holder must have "exclusive use" of 1Evidence that the airplaneis loaded according to 1at lease one aircraft for each operation authorized in the schedule. certificate holder's manual. 2Minimum fuel supply. 2at least one aircraft that meets the requirements of the 3Company or organization name. specific operations authorized in the certificate holder's operations specifications. 5261 A dispatch release for a flag or domestic air carrier 3at least one aircraft that meets the requirements of at must contain or have attached to it least one kind of operation authorized in the certificate 1weather information for the complete flight. holder's operations specifications. 2weight and balance data 3a crew list 5276. Which document specifically authorizes a person to operate anaircraftinaparticulargeographic area? 5266. What information is required in the flight release for 1Certificate of designation. supplemental air carriers and commercial operators that is 2Air taxi operating certificato. not required in the dispatch release for flag and domestic air 3Operations specifications. carriers? 1Weather reports and forecasts. 5277. If previous arrangements have not been made by the 2Nemes of all mewmembers. operator, where can the procedures for servicing the aircraft be found? 3Minimum fuel supply. 1Certificate holders director of maintenance. 5270. Which documents are required to be carried aboard 2Certificate holder's manual. each flag air carrier flight? 3Part E of the certificate holder's operations specifica- 1Dispatch release and weight and balance release. tions. 2Load manifest and bight release. 3Dispatch release, load manifest, and flight plan.

30 20 5278. What document contains procedures that explain 5258. Procedures for keeping copies of the aircraft mainte- how the required return-to-service conditions have been nance log inthe aircraft and available to appropriate met? personnel shall be set forth in fCerlificate holder's manual. 1the cxtificate holder's manual. 2Mechanical Interruption Summary Repoli. 2the aircraft maintenance procedures handbook. 3Operations Inspections and Surveillance Procedures 3Part D of the operations specifications. Handbook 5287. Which person, other than the second in command, 5279. Who isresponsible for keeping copiesofthe may the pilot in command permit to manipulate the flight certificateholder's manual up to date with approved controls? changes or additions? 1When authorized by the certificate holder, a passenger 1Each employee of the certificate holder who is furnished who holds a pilot certificate appropriate for the aircraft a manual. 2An authorized FM safety representative who Is qualified 2Air Taxi /Commercial Technical Service. intheaircraft,andischeckingflightoperations. 3A representative of the Administrator assigned to the 3A pilot employed by an engineering firm who is certificate holder. authorized by the certificate holder to conduct flight tests. 5280. An aircraft may be operated in a foreign country by a FAR Part 135 open -e onlyif authorized to do so by 5288. The maximum altitude loss for a malfunctioning autopilot without an approach coupler is 45 feet. If the MDA 1an FM International Field Office. is 1,820 feet MSL and the touchdown zone elevation is 2the ICAO (InternationalCivilAviationOrganization). 1.294 feet, to which minimum altitude may you use the 3the foreign country. autopilot? 5291. Who is responsible for the preparation of a required 1-1,510 feet MSL load manifest? 2-1,339 feet MSL 1Dispatcher. 3-1,570 feet MSL 2Air carrier certificate holder. 5289. The maximum altitudelossfor a malfunctioning 3Company official specifically designated by the Adminis- autopilot with an approach coupler is 40 feet 7vmich trator. minimum altitude may the autopilot be used during an ILS 5282. Which Is not a required Item on the load manifest? approach in less than basic VFR conditions? 1Aircraft registration or flight number. 1-40 feet AGL 2 List of passenger names. 2-50 feet AGL 3Identification of crewnfembers. 3-80 feet AGL 5213. A certificate holder must keep copies of completed 5290. The maximum altitude loss for a particular malfunc- load manifests for at least tioning autopilot under approach conditions is 55 feet if the touchdown lone elevation is 571 feet and the MDA is 1-30 days. 1,100 feet, to which minimum altitude may you use this 2-90 days. autopilot? 3-80 days. 1-828 feet MSL 5284. Before each flight, who is directly responsible for 2-990 feet MSL. determining theairworthinessstatusof a mechanical 3-1,050 feet MSL irregularity previously entered in the aircraft maintenance 5291. The maximum altitudeloss specified for mahunction of a certain autopilot undercruise conditions is 50 feet 1Aircraft dispatcher. What is the lowest altitudethis autopilot may be used 2Une maintenance supervisor. en route? 3Pilot in command of next flight 1-550 feet AGL 8285. Where is the certificate holder required to list the 2 -600 feet AGL. name and title of each person authorized to exercise 3-500 feet AGL. operational control for a particular flight? 5292. What is the lowest altitude above the terrain that an 1Part B of the certificate holder's Operations Specifica- autopilot may be used during en route operations, if the tions. airplane flight manual specifies a malfunction under miss 2Attached to the load manifest for that flight. conditions? 3Certificate holder's manual. 1-100 feet 2-500 feet. 3-1,000 feet

21 31 5293. The altitudelogs for a particularmalfunctioning 5299. Which person may be carried aboard an aircraft autopilot with an approach coupler Is 00 feet If the reported without complying with the passenger- carrying requirements weather is below basic VFR minimums and an ILS approach of FAR Part 135? using the approach coupler Is to be used, what minimum altitude may be used? 1An authorized technical representative of an aircraft or engine company. 1-50 feet AOL 2A member of the United States diplomatic corps on an 2-60 feet AOL official courier mission. 3-100 feet AOL 3An individual who is necessary for the safe handling of animals on the aircraft 5294. An autopilot may be used in place of a second in command in any aircraft 5300. In a cargoonly operation, cargo must be loaded 1being operated in commuter air carrier service. 1so that it does not obstruct the aisle between the crew 2having a passenger seating configuration, excludingany and cargo compartments. pilot's seat, of 10 seats or more. 2in such a manner that at least one emergency or regular 3having a total seating capacity of more than eight seats exit is available to all occupants. and being operated in commuter air service. 3so thatallrequired flight crewmembers have reedy access to ail regular and emergency exits. 5295. Which is a condition that must be met by a commuter air carrier certificate holder to have an aircraft approved for 5301. Which is a requirement governing the carriage of operation with an autopilot system and no second in cargo? command? 1Cargo must be carried in an approved rack, bin, or 1The passenger seating configuration is 12 or less, compartment excluding any pilot seat 2Cargo not stowed in an approved bin must be secured 2The autopilot system is capable of operating the controls by a safety belt or approved tiedown device. to maintain flight and to maneuver the aircraft about the 3All cargo carried in the passenger compartment must be three axes. packaged and stowed ahead of the foremost seated 3The operation is restricted to VFR or VFR over-the-top. passenger.

5296. A commuter air carrier certificate holder plans to 5302. Which is a requirement governing the carriage of assign a pilot as pilot in command of an aircraft having eight carry-on baggage? passenger seats to be used in passenger-carrying operations. Which experience requirement must that pilot meet If 1All carry-on baggage must be restrained so that its the aircraft is to be flown with an autopilot andno second in movement is prevented during turbulence. command? 2Carry-on baggage must be stowed ahead of all seated occupants. 1-100 hours as pilot in command in the make and model. 3Pieces ofcarry -on baggage weighing more than 2-100 hours in the category, class, and type. 10 pounds must be carried in an approved rack or bin. 3-50 hours and 10 landings as pilot in command in the make and model. 5303. Ifcarry-on baggage or cargoiscarriedinthe passenger compartment, it must be 5207. Who may be allowed to carry a deadlyweapon on board an aircraft operated under FAR Part 135? 1stowed ahead of the foremost seated passengers. 2placed in an approved rack,bin, or compartment 1Official bodyguards attached to foreign legations. installed in the aircraft 2Security officers employed by corporate executives. 3so located that it does not obstruct the aisle between 5Employees of a municipality or state authorized tocarry the crew and passenger compartments. arras. 5304. The load manifest must be prepared prior to each 5291 Which restriction must be observed regarding the takeoff for carrying of cargo in the passenger compartment? 1any aircraftwith a passenger seating capacity of 1Cargo must be properly secured by a safety belt or other 10 seats or more. approved tiedown. 2multiengine aircraft only. 2All cargo must be carried in a suitable bin and secured 3all helicopters and large aircraft operated by a commuter to a passenger seat or the floor structure of the aircraft. air carrier. 3Cargo carried in passenger seats must be forward of all passengers. 5305. Which minimum passenger seatingconfiguration requires a second in command? 1-10 seats. 2-12 seats. 3-15 seats. 5306. A flight attendant crewmember is required on aircraft 5312. Which is a condition that must be met when a person having a passenger seating configuration, excluding any is administered medical oxygen in flight? pilot seat, of 1The distance between a person using merovil oxygen 1-15 or more. and any electrical unit must not be less than 5 feet. 2-20 or more. 2A person using oxygen equipment must be seated to 3-19 or more. avoid restricting access to, or use of, any required exit. 3A person being administered oxygen must be monitored 5307. Before each takeoff, the pilot in command of an by equipment that displays and records pulse and aircraft carrying passengers shall ensure that all passengers respiration. have been orally briefed on the 5313. Which requirement applies when oxygen is stored in 1location of normal and emergency exits, oxygen masks, liquid form? and life preservers. 2use of seatbelts, oxygen, and liferafta 1liquified oxygen is a hazardous material and must be 3use of seatbelts, smoking, and location of survival kept in an isolated storage facility. equipment 2The equipment used to store liquid oxygen must be included in the certificate holder's approved mainte- 5306. Before takeoff, the pilot in command of an aircraft nance program. carrying passengers shall ensure that all passengers have 3 Smoking is not permitted within 50 feet of stored liquid been orally briefed on the normal and emergency use of oxygen. 0:10114n 5314. Which is a pilot requirement for oxygen? 1regardless of the altitude at which the flight will operate. 2if the flight involves operations above 12,000 feet MSL 1Each pilotof apressurizedaircraftoperatingat 3if the flight involves operations at or above 10,000 feet 18,000 feet MSL and above shall have an approved MSL for more than 1 hour. quick-donning type oxygen mask. 2On pressurized aircraft requiring a flightcrew of two 5300. The oral preflight briefing required on passenger- pilots,both shallcontinuously wear oxygen masks carrying aircraft shall be wheneverthecabin pressurealtitude exceeds 12,000 feet MSL 1supplemented by an actual demonstration of emergency 3On unpressurized aircraft, flying above 12,000 feet MSL, exit door operation by a crewmember. pilots shall use oxygen continuously. 2presented in person by the pilotin command while another flight crewmember demonstrates the operation 5316. Which is a requirement for pilot use of oxygen in a of emergency equipment. pressurized airplane? 3conducted by the pilot in command or a crewmember and supplemented by printed cards for the use of each 1At altitudes of 18,000 feet MSL and above, each pilot passenger. shall have an approved -pick-donning oxygen mask. 2The pilot at the controls shall use oxygen continuously 5310. Which is a requirement regarding the carriage and any time the'-abin pressure attitudeis more then operation of oxygen equipment for medical use by passen- 12,000 feet gers? 3At altitudes above 20,000 feet MSL, the pilot at the controls must use an approved oxygen mask any time 1No person may smoke %V 10 feet of oxygen storage the other pilot is away from the duty station. and dispensing equipment 2When oxygen equipmentisused for the medical 5316. Above which altitude must at least one pilot at the treatment of a patient, the rules pertaining to emergency controls of a pressurized aircraft wear a secured and sealed exit access are waived. oxygen mask? 3No person may connect oxygen bottles or any other ancillary equipment until all passengers are aboard the 1-30,000 feet MSL aircraft and seated. 2-35,000 feet MSL. 3-41,000 feet MSL 5311. If a certificate holder deviates from the provisions of regulations which pertain to medical use of oxygen by 5317. Which is a requirement for flightcrew use of oxygen passengers, a complete report of the incident shall be sent masks in a pressurized cabin airplane? to the FM within 1At altitudes above FL2Es, one of the two pilots at the 1-48 hours. controls shall use an oxygen mask continuously. 2-7 working days. 2Both pilots at the controls shall use oxygen masks 3-10 working days. above FL300. 3At altitudes above 25,000 feet MSL, if one pilot leaves the pilot duty station, the remaining pilot at the controls shall use an oxygen mask.

23 33 5319. At altitudes above 10,000 feet through 12,000 feet 5324. Which performance requirement applies to passen- MSL, each pilot of an unpressurized airplanemust use ger-canying land airplanes being operated over water? supplementsl oxygen for that part of the flight that isof a duration of more than 1 Muftiengine airplanes must be able to climb, with the critical engine inoperative, at least 100 feet a minute at 1-20 minutes. 1,500 feet above the surface. 2-30 minutes. 2Single-engine airplanes must be operated at an altitude 3-45 minutes. that will allow them to reach land in case of engine failure. 5319. The two pilot stations of a pressurized aircraftare 3Both single - engine and multiengine airplanes must have equipped with approved quick-donning oxygen masks. What integral flotation devices that will keep them afloat in Is the maximum altitude authorized without one pilot wearing event of ditching. and using an oxygen mask? 1-25,000 feet MSL 5325. The weight and CG of an aircraft used in air taxi 2-35,000 feet MSL service must have been calculated from those values 3-41,000 feet MSL ostablished by actual weighing of the aircraft within what period of time? 5320. In airplanes where a third gyroscopic bank-and-pitch 1Multiengine aircraft, 24 calendar months; single-engine, indicator is required, that instrument must 36 calendar months. 1continue reliable operation for at least 45 minutes after 2Multiengine aircraft, 36 calendar months. the output of the airplane's electrical generating system 3 Muftiengineandsingle-engineaircraft,36 calendar fails below an optimum level. months. 2be operable by a selector switch whichmay be actuated from either pilot station. 5326. Which aircraft must be equipped with an approved public address and crewmember interphone system? 3continue reliable operation for a minimum of 30 minutes after total failure of the aircraft's electrical generating 1All turbine-engine-powered aircraft in passenger-carrying system. operations. 2Aircraft having a passenger seating configtration, ex- 5321. In which aircraft operating under FAR Part 135 is a cluding any pilot seat, of more than 19 seats. third gyroscopic bank-and-pitch indicator required? 3Multiengine aircraft having a passenger seating configu- 1All turbojet airplanes. ration of 10 seats or more. 2All airplanes where the flIghtcrew of pilot incommand and second In command are required. 5327. Information recorded during normal operations by a required cockpit voice recorder 3All airplanes having a passenger seatingcapacity of 30 seatsOfmore. 1must be retained for at least 12 hours. 2may be erased only once each flight. 5322. To operate a multiengine aircraft with certain equip- 3may be erased, except the last 30 minutes. ment inoperative under the provisions ofa minimum equipment list, what document must be carried withinthe 5326. An approved cockpit voice recorderisrequired aircraft? equipment in

1Letter from the Regional Airworthiness Office authorizing 1large airplanes having a maximum passenger capacity of such operation. more than 19 seats. 2Letter from the certificate holder's director of mainte- 2turbojet-powered airplanes having a passenger seating nance authorizing the operation. configuration, excluding any pilot seat, of 10 seats or 3Letter of Authorization Issued by the FAA districtoffice more. having certification responsibility. 3all aircraft operated in commuter air carrier service having a passenger seating configuration of 19 seats or 5323. What performance isrequiredof a multiengine more. airplane with the critical engine inoperative, while carrying passengers for hire in IFR weather conditions? 5329. During vn ich time period must a required voice recorder of a passengercarrying airplane be continuously 1Climb at least 100 feet a minute at the highest MEAof the route to be flown or 3,000 feet MSL, whichever is operatr d? higher. 1From the beginning of taxi to the end of the landing roll. 2Climb at least 50 feet a minute at the MEA's of the 2From engine sten at departureairportto engine route to be flown or 5,000 feet MSL, whichever is shutdown at landing airport. higher. 3From the use of the checklist before the flight to 3Maintain altitude at the highest MEA of the route to be completion of the final check at the end of the flight. flow, or 5,000 feet MSL, whichever is higher.

24 5330. In which airplanes Is a ground proximity warning 5336. An unpressurized aircraft with 10 occupants other system required? than the pilots,will be cruising at 11,000 feet MSL for 20 minutes. For how many, if any, of these occupants must 1M airplanes having a passenger seating configuration, there be an oxygen supply? excluding any pilot seat, of 10 seats or more. 2Airplanes having a passenger seating configuration of 1Five. 19 seats or more, tekig operated In commuter air 2One. swim 3None. 3Turbojet-pownad airplanes having a passenger seating configuatton, excluding arn pilot seat, of 10 seats or 5337. The oxygen requirements for occupants of a pressur- more. ized airplane operated at altitudes above 24,000 feet MSL is dependent upon the airplane's ability to descend safely to 5331. When a ground proximity warning system is required an altitude of under FAR Part 135, It must 1-10,000 feet MSL in 4 minutes. 1convey warnings for excessive closure rates with the 2-15,000 feet MSL in 4 minutes. terrain but not for deviation from an ILS glide slope. 3-12,000 feet MSL at a minimum rate of 2,500 ft/min. 2alert the pilot by an audible warning signal when deviation above or below glide slope occurs. 5336. In addition to fully-equipped liferafts and life preserv- 3convey warnings of any deviation below glide slope and ers, what emergency equipment must be provided during of excessive closure rate with the terrain. extended overwater operations?

5332. When a ground proximity warning system is required, 1One water resistant, self-buoyant, portable emergency radio transmitter for each 10 occupants. it must 2One survival-type emergency locator transmitter. 1Incorporate a means c alertingthepilot when a 3One pyrotechnic signaling device for each 10 occupants. malfunction occurs. 2apply corrective control pressure when deviation below 5339. Which is a requirement for life preservers during glide slope occurs. extended overwater operations? Each life preserver must be 3Incorporate a backup feature that activates automatically equipped with upon total failure of the aircraft's electrical generating 1an approved survivor locator light %stem. 2a dye marker. 5333. A pressurized airplane being operated at FL300 can 3one flashlight having at least two size "D" cells or descend safely to 15,000 feet MSL in 4 minutes. What equivalent. oxygen supply must be carried for all occupants other than 5340. Which aircraft must have a shoulder harness installed the pilots? at each flight crewmember station? 1-30 minutes. 1Aircraft having a passenger seating configuration, ex- 2-45 minutes. cluding any pilot seat, of 10 seats or more. 3-1 hour. 2All passenger-carryingaircraftoperating under FAR 5334. Above what altitude in an unpressurized airplane, Part 135. must all passengers be supplied oxygen? 3Large aircraft being operated in commuter air service. 1-12,000 feet MSL 5341. Under which condition is a pilot not required to keep 2-14,000 feet MSL the shoulder harness fastened during takeoff and landing 3-15,000 feet MSL while at a pilot station?

5335. Between what altitudes in an unpressurized airplane 1When operating an aircraft having a passenger seating mub, oxygen be available to at least 10 percent of the configuration, excluding any pilot seat, of 10 seats or occupants, other than the pilots? less. 2When the pilot cannot perform the required duties with 1Above 10,000 feet through 15,000 feet MSL, if flight at the shoulder harness fastened. those altitudes is of more than a 30-minute duration. 3When serving as pilotin command or second in 2Above 12,000 feet through 16,000 feet MSL, for any command of an aircraft having a total seating capacity of time period. eight seats or less. 3Above 12,000 feet through 15,000 feet MSL, if flight at those altitudes is of more than a 15-minute duration. 5342. Which airplanes must have a shoulder harness installed at each flight crewmember station? 1All airplanes operating under FAR Part 135. 2All turbojet-powered airplanes. 3All airplanes used in commuter air service.

25 35 5343. In which aircraft, or under what conditions, is airborne 5349. Walch condition must be mettr;conduct IFR thunderstorm detection equipment required? operations from an airport that is not at the location where weather observations are made? ltiengine turbine-powerd aircraft havinga passenger seating configuration of 19 seatsor more being oper- 1The Administrator must issue operations specifications ated by a commuter air carrier. that permit the procedure. 2Any aircraft having a passenger seatingconfiguration of 2A "Letter of Waiver" authorizing the procedure must be 19 seats or more that Is engaged in passenger-carrying Issued by the U.S. National Weather Service. creations under IFR or at night 3An "Authorization Letter" permitting the procedure must 3Small multiengine aircraft havinga passenger seating be issued to the operator by the supervising FM district configuration of 10 seats or more, excludingany pilot office. seat, that are engaged in passenger- carrying operations. 5350. What are the empty weight and balancecurrency 5344. Airborne weather radar equipment mustbe installed requirements for aircraft used in air taxi service? in large transport category aircraft in the conterminous 48 United States 1The empty weight and CG of multiengine and single- engine aircraft must have been calculated froman actual 1and be fully operational, although weather forecasts weighing within the previous 24 calendar months. Indicate no hazardous conditions. 2The empty weight and CG of multiengine aircraftmust 2engaged in passenger-carrying operations. 3engaged have been calculated from an actual weighing within the In either cargo or passenger-carryingoper- previous 38 calendar months. ations. 3The empty weight and CG must have been calculated from an actual weighing within the previous 24 calendar 5345. An aircraft has a passenger seating configurationof 18 seats, excluding any pilot seats. How months unless the original Airworthiness Certificatewas many, if any, issued within the previous 38 calendar months. approved first aid kits are required? 1One. 5351. A pilot may not begin an IFR operation unless the 2Two. next airport of Intended landing Is forecast to be at or above 3None. authorized IFR landing minimums at 1the estimated time of arrival. 53411. How many, If any, approved first aid kitsare required on an aircraft having a passenger seating configuration of 2the estimated time of arrival, plus or minus 1 how. 20 seats and a passenger load of 14? 3-30 minutes before, until 30 minutes after, the estimated time of arrival. 1None. 2One. 5352. A takeoff may not be made from an airport that is 3Two. below the authorized IFR landing minimums unless

5347. When a crash ax is 1there Is an alternate airport with the required IFR landing required equipment on an minimums within 45 minutes' flying time. aircraft, where should it be located? 2the departure airport is forecast to have the required IFR 1As close as practicable to anemergency exit. landing minimums within 1 hour. 2At a location where it is inaccessibleto the passengers 3there Is an alternate airport with the required IFR landing during normal operations. minimums within 1-hour's flying time. 3At a location where it Is accessibleto both the crew and passengers during normal operations. 5353. A pilot may not designate an airport as an alternate unless it is forecast to be at or above alternate minimums at 5345. A pilot may make an IFR departure from an airport 1the time of departure. that doss not have an approved standardinstrument approach procedure if the 2the estimated time of arrival, plus or minus 1 hour. 3the estimated time of arrival. 1certificate holder holds a waiver from ATCapproving the procedure. 5354. Assuming the required ceiling exists, an alternate for 2certificate holder has been issued operationsspecifica- the destination airport Is not required if, for at least 1 hour tions by the Administrator approving theprocedure. before and after the ETA, the forecast visibility Is at least 3deparkze airport is within 30 minutesor less flying time 1-5 miles, or 3 miles more than the lowest applicable of another airport that has an approved standard visibility minimums for the instrument approachproce- instrument approach procedure. dure to be used, whichever is greater. 2-3 miles, or 2 miles more than the lowest applicable visibility minimums for the instrument approachproce- dure to be used, whichever Is greater. 3-5 miles, or 3 miles more than the lowest applicable circling minimums. 36 _20 5355. The requiredvisibilityexists and circlingisnot 5362. After passing the final approach fix on a VOR authorized. An alternate for the destination airport is not approach, a weather reportisreceived indicating the required if, for at least 1 hour before and after the ETA, the visibility is below prescribed minimums. In this situation, the forecast ceiling is at least pilot 1-1,500 feet above the lowest published minimum, or 1may continue the approach and land, if at the MDA the 2,000 feet above the airport elevation, whichever is visibility is at least equal to the required minimums. higher. 2should continue the approach to the MDA, and regard- 2-1,000 feet above the lowest MEA, MOCA, or attitude lessof thevisibility,execute a missed approach. prescribed for the initial approach procedure for the 3continue the approach and land regardless of the airport. visibility you observe at the MDA, if prior to beginning the 3-1,000 feet above the lowest published minimum, or approach,thevisibility was reportedat or above 1,500 feet above the airport elevation, whichever is minimums. higher. 5363. Which is one required condition for a pilot to take off 5356. If the weather forecasts do not require the listing of under IFR with less-than-standard takeoff minimums at an an alternate airport on an IFR flight, the airplane must carry airport where a straight-in instrument approach procedure is sufficient fuel to fly to the destination airport and authorized and there is an approved weather reporting source? 1fly thereafter for 45 minutes at normal cruising speed. 2fly thereafter for 30 minutes at normal cruising speed. 1The pilot must have at least 100 hours as phut in 3make one missed approach and thereafter have a command in the type airplane to be flown. 45-minute reserve at normal cruising speed. 2Visibility at time of takeoff must be at least RVR 16. 3Wind direction and velocity must be such that a straight- 5357. If the weather forecasts require the listing of an in approach can be made to the runway served by the alternate airport on an IFR flight, the airplane must carry procedure. enough fuel to fly to the first airport of intended landing, then to the alternate, and fly thereafter for a minimum of 5364. Which is an operational requirement concerning ice, snow, or frost on structural surfaces'? 1-30 minutes. 2-20 minutes. 1A takeoff may not be made if ice or snow is adhering to 3-45 minutes. the wings or stabilizing or control surfaces. 2A takeoff may be made with ice, snow, or frost adhering 535$. At a foreign airport, a pilot may not take off under to the wings or stabilizing or control surfaces if anti-icing IFR unless the reported weather conditions indicate that the and deicing equipment is operating. 1--visibility is 1 mile or more. 3If snow, ice, or frost is adhering to the airplane's lift or 2ceiling is at least 500 feet and the visibility is 1 mile or control surfaces, but polished smooth, a takeoff may be more. made. 3visibility is 1/2 mile or more. 5365. What are the minimum certificate and rating require- 5359. A pilot may not take off under IFR at a military airport ments for the pilot in command of a multiengine airplane in unless the visibility is commuter air carrier service under IFR? 1at least 1 mile. 1Airline transport pilot of any category; multiengine class 2-1/2 mile or more. rating. 3-3/4 mile or more. 2Airline transportpilot;airplane category; multiengine class rating; airplane type rating, if required. 5360. A pilot may not make an instrument approach at a 3Commercial pilot airplane category; muitiengine class military or foreign airport unless the minimum visibility is at and instrument rating. least 5366. A multiengine airplaneisbeing operated by a 1-1/2 mile. commuter air carrier. What are the minimum certificate and 2RVR 32. rating requirements for the pilot in command? 3RVR 40. 1Airline transportpilot;airplane category; multiengine 5161. An instrument approach procedure to an airport may class; airplane type rating, if required. not be initiated unless the latest weather report issued by an 2Commercial pilot; airplane category; multiengine class; authorized weather reporting facility indicates that weather instrumentrating;airplanetyperating,ifrequired. conditions 3Airline transportpilot;airplane category;multiengine class. 1are at or above the circling minimums for the runway the pilot intends to use. 2exceed the straight-in minimums for all nonprecision approaches. 3are at or above the authorized IFR landing minimums for that procedure.

577 5357. What are the minimum certificate and rating require- 5373. What Instrument time experience musta pilot have ments for the pilot in command of a turbojet airplane with had to act as second in command of an airplane foran IFR two engines? air bud flight? 1Airline transport pilot of any category;multiengine class 1-8 hours of actual or simulated instrument flight time rating airplane type rating. within the preceding 6 months. 2Airline transport pilot airplane category; multiengine 2-3 hours of instrumentflighttime under actual or class rating; airplane type rating, If required. simulated instrument flight conditions within the preced- 3Commercial pilot airplane category; multiengine class Inp 6 months. rating instrument rating; airplane type rating. 3-3 hours of actual or simulated instrument flight time within the preceding 90 days. 5368. A person is designated pilotin command of a mudengine, reciprocating-engine-powered airplane operated 5374. To satisfy the instrument approachrecency experi- in passenger-carrying service bya commuter air carrier. If ence requirement, a second in command must have made five takeoffs and landings are accomplishedin that make at least and basic model, which additional pilot-in-commandexperience meets the requirement for designation? 1six approaches within the past 6 months; threemust have beeninthecategoryaircraftto be flown. 1Two takeoffs and landings, and 8 hours. 2six approaches within the past 6 months inany airplane, 2Five takeoffs and landings, and 5 hours. helicopter, approved instrument ground trainer,or simu- 3Three takeoffs and landings, and 6 hours. lator. 3three approaches within the past 90 days inan airplane, 5350. A person is designated as pilot incommand of a helicopter, approved instrument ground trainer,or simu- turbojet-powered airplane operated in passenger-carrying lator. service by a commuter air carrier.If 10 takeoffs and landings are accomplished in that make and basic model, 5375. Pilot flight time limitations under FAR Part 135are which additional pilot-in-command experiencemeets the based requirement for designation? 1on the flight time accumulated under FAR Part 135 and 1-10 hours. in any other commercial flying. 2-10 hours, and five takeoffs and landings. 3-15 hours. 2solely on flight time accumulated in air taxi operations. 3solely on flight time accumulated under FAR Part 135 and FAR Part 121. 5370. A pilot's experience Includes 8 hoursin a particular make and basic model multiengine, turbopropairplane. 5378. A person may not serve as pilot in any operation Which additional pilot-in-command experiencemeets the unless that person has passed requirements for designation as pilot in commandof that airplane when operated by a commuterair carrierin 1a competency check within 180 days prior to the dateto passenger-carrying service? serve. 2an aircraft proficiency check since the beginning of the 1Five takeoffs and landings, and 2 hours. 8th calendar month prior to the date to serve. 2Ten takeoffs and landings, and 2 hours. 3a competency check sincethe beginningof 3Twelve takeoffs and landings. the 12th calendar monthpriortothe dateto serve. 5371. A person Is designated pilot In command of a single- 5377. A pilot in command who is authorized touse an engine airplane operated In passenger-carryingservice by a autopilot system in place of a second in command, commuter air carrier. may If seven takeoffs and landingsare take the autopilot check accomplished Inthat make and basicmodel, which additional pilot-in-command experiencemeets the require- 1concurrently with the instrument proficiency check, but at ment for designation? 1-month Intervals. 1-5 hours. 2in any aircraft appropriately equipped, providing the check is taken at 3-month intervals. 2-8 hours. 3-10 hours. 3concurrently with the competency check, providing the check is taken at 6-month intervals. 5372. A person is designated pilot in command of a 5378. A person may not serve as pii.4 in command inan multiengine, turboprop-powered airplane operatedIn pas- IFR operation unless that person has passedan senger-canying service by a commuter air carrier.If eight takeoffs and landings are accomplished inthat make and 1aircraft competency and an Instrument proficiency check basic model, which additional pilot-in-commandexperience within the previous 16 calendar months. meets the requirement for designation? 2Instrument proficiency check in the airplane In whichto serve, or in an approved aircraft simulator, within the 1-7 hours. previous 12 calendar months. 2-5 hours, and two takeoffs and landings. 3 instrument proficiency check under actualor simulated 3-10 hours, and two takeoffs and landings. IFR conditions, since the beginning of the 6th calendar month prior to the date to serve.

;26 38 5370. A person is assigned as pilot in command to fly both 5384. To serve as pilot in command in an IFR operation, a single-engine and multiengine airplanes and has passed the person must have passed a line check initial Instrument proficiency check in a multiengine airplane. 1since the beginning of the 12th month before that Which requirementappliesregarding each succeeding service, which included at least one flight over a civil instrument check? airway, or approved off-airway route, or any portion of 1The instrument check must be taken each 6 calendar either. months inboth a single-engine and a mualengine 2-- consisting of a flight over the route to be flown, with at akplane. least three instrument approaches at representative 2The instrument check must be taken alternatelyin airports, within the past 12 calendar months. single-engine and multiengine airplanes. 3within the past 12 months, which Include a portion of a 3The instrument check may be taken in either a single- civilairway and one instrument approach at one engine or multiengine airplane if taken at intervals of representative airport 3 calendar months. 5385. Which takeoff computation must not exceed the 5380. A pilot in command is authorized to use an autopilot length of the runway plus the length of the stopway for a system in place of a second in command. During the turbine-engine-powered small transport category airplane? instrument proficiency check, that person is required to 1Takeoff distance. demonstrate the ability to 2Acceleration-stop distance. 1properly conduct instrument operations competently both 3Takeoff run. with, and without, the autopilot 2properly conduct air-ground communications with, but 5388. The effective length of the most favorable runway at not without, the autopilot a certainairportis8,600 feet. The maximum landing 3comply with complex air traffic control instructions with, distance permitted for a large transport category turbopro- but not without, the autopilot peller-powered airplane to list this airport as an alternate is 1-6,020 feet 5381. A person may act as pilot in command of both type A and type B aircraft under IFR if an instrument proficiency 2-6,880 feet 3-7,740 feet check has been passed in 1type A since the beginning of the 12th month, and in 5387. What is the maximum landing distance for a turbojet type B since the beginning of the 6th month before time small transport category airplane if the effective length of to serve. the most favorable runway of the airport to be used as an 2either type A or B since the beginning of the 24th month alternate is 8,000 feet? before time to serve. 1-6,400 feet 3type A since the beginning of the 12th month, and in 2-5,600 feet type B since the beginning of the 24th month before 3-4,800 feet. time to serve. 5388. What is the maximum landing distance for a turbine- 5382. No certificate holder may use a person as pilot in engine-powered small transport category airplaneif the command unless that person has passed a line check effective length of the most favorable runway of the 1within the past 180 days. destination airport is 7,000 feet? 2since the beginning of the 6th month before serving as 1-4,200 feet pilot in command. 2-4,900 feet. 3since the beginning of the 12th month before serving as 3-5,600 feet pilot in command. 5389. Ifacertificateholder makes arrangements for 5383. What are the minimum requirements for the line another personto performaircraftmaintenance, that check required of each pilot In command authorized for IFR maintenance shall be performed in accordance with the air taxi operations? The line check shall be given over 1 certificate holder's manual and FAR Parts 43, 91, and 1one route segment in each type of airplane the pilot is to 135. fly and Includes takeoffs and landings at each airport on 2provisions of a contract prepared by a certificate holder the route. and approved by the supervising FM district office. 2a civil airway or an approved off-airway route In one type 3provisions and standards outlinedinthe certificate of airplane the pilot is to fly and includes takeoffs and holder's aircraft maintenance handbook. landings at one or more representative airports. 3a civil airway or an approved off-airway route in each make and model airplane the pilot is to fly and Includes instrument approaches at each designated airport on the route. 5390. Who isresponsible for submitting a Mechanical 5398. The aircraft operator discovers that the label on a Reliability Report? container of hazardous material is missing. How should the appropriate replacement label be determined? (See appen- 1-Air carrier and commercial operator certificate holders. dix 2, Excerpt from CFR 49, Part 175.) 2-Maintenance fricility that discovers a reportable condition. 1-Shipping papers. 3-Aircraft maintenance inspector at districtoffice that 2-Hazardous material index. exercises surveillance. 3-Hazardous materials table of CFR 49.

6391. If not excepted, what label, if any, must be placed on 5399. An operator makes a telephone report of an incident a package containing acetone? (See appendix 2.) involving fire during the loading of hazardous materials. 1-No label is required. Within what period of time must a written report be 2-POISON. submitted? (See appendix 2, Excerpt from CFR 49, Part 175.) 3- FLAMMABLE LIQUID. 1-48 hours. 5392. What is the maximum, if any, net quantity of acetyl 2-10 days. bromide in one package, that may be carried in a cargo-only 3-15 days. aircraft? (See appendix 2.) 1-1 quart. 5400. Which procedure must be followed if an operator, 2-1 gallon. when loading magnetized material, cannot avoid placing it in a position where it affects the accuracy of the magnetic 3-No limit is specified. compass? (Seeappendix2,Excerptfrom CFR 49, Part 175.) 5393. What isthe maximum,ifany,net quantity of acetylene in one package, that may be carriedin a 1-Placard the compass "unreliable." passenger - carrying aircraft? (See appendix 2.) 2-Rely solely on electronic navigation. 1-Any amount is forbidden. 3-Make a special compass swing and calibration. 2-300 pounds. 3-No limit is specified. 5401. Which class of hazardous material must be loaded aboard an aircraft in a position that allows no contact with 6394. If not excepted, what label, if any, must be placed on containers of corrosive materials? (See appendix 2, Excerpt a package containing allethrin? (See appendix 2.) from CFR 49, Part 175.) 1-ORM-A. 1-Organic chemicals. 2-None. 2-Oxidizing materials. 3-CORROSIVE. 3-Catalytic agents.

5395. What isthe maximum,ifany,net quantity of 5402. What is the maximum weight of hazardous material aluminum hydride in one package, that may be carried in a (other than nonflammable compressed gas) that mny be passenger-carrying aircraft? (See appendix 2.) carried in an accessible cargo compartment of a passenger- carrying aircraft? (See appendix 2, Excerpt from CFR 49, 1-No limit is specified. Part 175.) 2-25 pounds. 3-Any amount is forbidden. 1-50 pounds, unless otherwisespecificallypermitted. 2-10 pounds, if classified as corrosive. 5398. Hazardous material shipped in an aircraft operated 3-25 pounds, if classified as ORM-D. under FAR Part 135 must be described and certified on a shipping paper. For what period of time must the originating 5403. What is the maximum, if any, number of packages of aircraft operator retain one copy c I this document? (See OR M material that may be transported in a passenger- appendix 2, Excerpt from CFR 49, Part 175.) carrying aircraft? (See appendix 2, Excerpt from CFR 49, Part 175.) 1-30 days. 2-130 days. 1-No limit applies 3-90 days. 2-A number whose combinedtransportationindices total 50. 5397. Certainclasses of hazardousmaterial may be 3-A number whose combinedtransportationindices shipped by air but are not permitted aboard passenger- total 100. carrying aircraft. How must such material be labeled? (See appendix 2, Excerpt from CFR 49, Part 175.) 5404. If transported in a passenger-carrying aircraft, what is the maximum combined transportation indices of packages 1-DANGEROUS. containing radioactive material .? (See appendix 2, Excerpt 2-HAZARDOUS/CLASS X. from CFR 49, Part 175.) 3-CARGO AIRCRAFT ONLY. 1-100. 2-50. 3-25. AO 5405. What is the maximum quantity of flammable liquid 5413. For a given angle of bank, the load factor imposed fuelthat may be carriedinthe cabinof a small, on both the aircraft and pilot in a coordinated constant nonscheduled, passengeroanylng aircraft being operated In altitude turn a remote area of the United States? (See appendix 2, Excerpt from CFR 49, Part 175.) 1Is directlyrelatedtotheairplane'sgross weight 2varies with the rate of turn. 1-10 gallons. 3Is constant 2-15 gallons. 3-20 gallons. 5414. What is the ratio between the total air load imposed on the rotor disc and the gross weight of a helicopter in MOIL What is the minimum distance that a package of radioactive materials bearing the label "RADIOACTIVE YELLOW II," and having a transport index of 15, may be 1Power loading. placed from a space continuously occupied by people? (See 2Load factor. appendix 2, Excerpt from CFR 49, Part 175.) 3Aspect ratio. 1-9 feet 5415. If an aircraft with a gross weight of 2,000 pounds 2-4 feet were suspected to a total load of 6,000 pounds in flight, the 3-5 feet load factor would be 5407. Who should be notifiedIf there is a suspected 1-2 O's. admen contemlnation involving a radioactive materials 2-3 0's. shipment and It is determined that radiological advice is 3-9 0's. needed? (See appendix 2, Excerpt from CFR 49, Part 175.) 541$. What does wing loading during a level coordinated 1 Office of Haire Ps Materials Regulation. turn in smooth air depend upon? 2U.& Energy Research and Development Administration. 1 Rate of turn. 3Nuoiser Regulatory Commission. 2Angie of bank. 5409. What precaution, If any, should be taken If dry Ice is 3True airspeed. carried aboard an aircraft? 5417. What is the relationship of the rate of turn with the 1This material does not require special precautions. radius of turn with a constant angle of bank but increasing 2A waiver to carry this material should be requested from airspeed? the certificating FM district office. 1Rate will decrease and radius will increase. 3Proper ventilation of the aircraft should be assured. 2Rate will increase and radius will decrease. 54011. How can turbulent air cause an increase in stalling 3Rate and radius will increase. speed of an airfoil? 541%. How can the pilot increase the rate of turn and 1An abrupt change in relative wind. decrease the radius at the same time? 2A decrease in angle of attack. 1Steepen the bank and Increase airspeed. 3Sudden decrease in load factor. 2Steepen the bank and decrease airspeed. 5410. What effect does an increase in airspeed have on a 3Shallow the bank and increase airspeed. coordinated turn while maintaining a constant angle of bank 5419. Why must the angle of attack be increased during a and attitude? turn to maintain altitude? 1The rate of turn will decrease resulting in a decreased 1Compensate for loss of vertical component oflift. load factor. 2Increase the horizontal component of lift equal to the 2The rate of turn will increase resulting in an increased vertical component. load factor. 3Compensate for increase in drag. 3The rate of turn will decrease resulting in changes in load factor. 5 420. If no corrective action is taken by the pilot as angle of bank is increased, how is the vertical component of lift 5411. What is the effect on total drag of an aircraft if the and sink rate affected? airspeed decreases in level flight below that speed for miodmum VD? 1Uft increases and the sink rate increases. 2Uft decreases and the sink rate decreases. 1Drag increases because of inn -eased induced drag. 3 Lift decreases and the sink rate increases. 2Drag increases because of Inc, eased parasite drag. 3Drag decreases because of lower induced drag. 5421. What affects indicated stall speed? 5412. What is load factor? 1Weight, load factor, and power. 2Load factor, angle of attack, and power. 1Uft multiplied by the total wiolht 3Angle of attack, weight, and air density. 2Uft subtracted from the total weight 3UN dMded by the total weight 0141 5422. In a light twin-engine airplane withone engine 5430. Under what condition is Vmc the highest? inoperative, when is it acceptable to allow the ball ofa slip- skid indicator to be deflected outside thereference lines? 1Gross weight isat the maximum allowablevalue. 2CG is at the most rearward allowable position. 1While maneuvering at minimum controllableairspeed to 3CG is at the most forward allowable position. avoid overoanidng. 2When operating at any airspeedgreater than Vim, 5491. What action should be taken ifone engine of a light 3When practicing imminent stalls ina banked attitude. twin-engine airplane becomes inoperative prior to lift-off during takeoff? 5423. What is the safest and most efficienttakeoff and initialclimb procedure in a light twin-engine airple ne? 1Accelerate to Vyn before lift -off. Accelerate to 2Accelerate to Vm before lift -off. 3Close both throttles and abandon the takeoff. 1best engine-out, rate-of-climb airspeed whileon the ground, then lift off and climb at that speed. 5432. What is the resulting performance loss whenone 2Vm, then lift off at that speed and climb atmaximum engine on a twin-engine fails? angle-of-climb airspeed. 3an airspeed slightly above Vide, then lift off and climbat 1Reduction of cruise airspeed by 50 per ant the best rate-of-climb airspeed. 2Reduction of climb by 50 percent or more. 3Reduction of all performance by 50 percent. 5424. What procedure is recommended foran engine-out approach and landing? 5433. When an engine falls after takeoff, what technique will provide the best climb performance? Wings be', clued 1The flightpath and procedures should be almostidentical approximatelyrtoward the to a normal approach and landing. 2The altitude and airspeed should be considerablyhigher 1Inoperative engine and the ball centered. ti.an normal throughout the approach. 2operating engine and the ball centered. 3A normal approach, except do not extend thelanding 3operating engine and ball displacedone diameter toward gear or flaps until over the runway threshold. the operating engine.

5425. What performance should a pilot ofa light twin- 5434. If an engine failure occurs at an altitude above single- engine airplane be able to maintain at Vmc? engineceiling,what airspeedshould be maintained? 1HeadIng. 1Vue. 2Heading and altitude. 2Vyn. 3Heading, altitude,andabilitytoclimb50ft /min.

5426. What criteria determines which engineis the "criti- 5435. What is the reason for variations in geometric pitch cai" engine of a twin-engine airplane? (twisting) along a propeller or rotor blade? 1The one with the center of thrust closestto the 1It permits a relatively constant angle of attack along its centerline of the fuselage. length when in cruising flight 2The one designated by the manufacturerwhich develops 2 It prevents the portion of the bladenear the hub or root most usable thrust from stalling during cruising flight. 3The one with the center of thrust farthestfrom the 3It permits a relatively constant angle of incidence along centerline of the fuselage. Its length when in cruising flight.

5427. What effect, if any, does altitude haveon Vmc for an 5436. Describe dynamic longitudinal stability. airplane with unsupercharged engines? 1Motion about the longitudinal axis. 1None. 2Motion about the lateral axis. 2 Increases with altitude. 3Motion about the vertical axis. 3Decreases with altitude. 5437. What is a characteristic of longitudinal instability? 5425. Under what condition should stalls never be practiced 1 Pitch oscillations becoming progressively greater. in a twin-engine airplane? 2Rank oscillations becoming progressively greater. 1With one engine inoperative. 3- craft constantly tries to pitch down. 2 With climb power on. --With full flaps and gear extended. 6436. Identify the typestabilityiftheaircraftattitude remains in the new position after the controls have been 5429. The blue radial line on the airspeed indicatorof a neutralized. light twin-engine airplane represents 1Negative longitudinal static stability. 1maxlmum single-engin', rate of climb. 2Neutral longitudinal dynamic stability. 2maximum single-engine angle of climb. 3Neutral longitudinal stedc stability. 3minimum controllable airspeed for single-engineoper- ation. 3242 5439. Identify the type stability if the aircraft attitude tends 5447. What performanceischaracteristicofflightat to move farther from its original position after the controls maximum L/D in a propellertiven airplane? have been neutralized. 1Maximum range and distance glide. 1Negative static stability. 2Best angle of climb. 2Positive static stability. 3Maximum endurance. 3Negative dynamic stability. 5448. On an airfoil, the force of lift acts perpendicular to 5440. Identify the type stability if the aircraft attitude tends and the force of drag acts pare" 1 to the to return to its original position after the controls have been 1chord line. neutralized. 2flightpath. 1Positive dynamic stability. 3longitudinal axis. 2Positive static stability. 3Neutral dynamic stability. 5449. By changing the angle of attack of a wing, the pilot can control the airplane's 5441. What effect does landing at high elevation airports 1 lift, gross weight, and drag. have on groundspeed with comparable conditions relative to 2 lift, airspeed, and drag. temperature, wind, and airplane weight? 3lift and airspeed, but not drag. 1Higher than at low elevation. 2 Lower than at low elevation. 5450. Which maximum range factor decreases as weight 3The same as at low elevation. decreases?

5442. What flight condition should be expected when an 1Angle of attack. aircraft leaves ground effect? 2Altitude. 3Airspeed. 1An Increase in induced drag requiring a higher angle of attack. 5451. What are some characteristics of an airplane loaded 2A decrease in parasite drag permitting a lower angle of with the CG at the aft limit? attack. 1Lowest stall speed, highest cruise speed, and least 3An increase in dynamic stability. stability. 2Highest stall speed, highest cruise speed, and least 5443. What characteristic should existif an airplane is loaded to the rear of its CG range? stability. 3Lowest stall speed, lowest cruise speed, and highest 1Sluggish in aileron control. stability. 2Sluggish in rudder control. 3Unstable about the lateral axis. 5452. The lift differential that eZzits between the advancing main rotor blade and the retreating main rotor blade is 5444. What will be the ratio between airspeed and lift if the known as angle of attack and other factors remain constant and airspeed Is doubled? Lift will be 1Coriolis effect. 2dissymmetry of lift. 1the same. 3translating tendency. 2two times greater. 3four times greater. 5453. During a hover, a helicopter tends to drift in the direction of tail rotor thrust. What is this movement called? 5445. What true airspeed and angle of attack should be used to generate the same amount of lift as altitude is 1Translating tendency. Increased? 2Transverse flow effect. 3Gyroscopic precession. 1The same true airspeed and angle of attack. 2A higher true airspeed for any given angle of attack. 5454. What is the purpose of the lead-lag (drag) hang, in a 3A lower true airspeed and higher angle of attack. three-bladed,fullyarticulatedhelicopterrotorsystem?

544d. How can an airplane produce the same lift in ground 1Offset lateral instability during autorotation. 2Compensate for Coriolis effect effect as when out of ground effect? 3Provide geometric balance. 1The same angle of attack. 2A lower angle of attack. 5455. During an autorotation (collective pitch full down), 3A higher angle of attack. whatisan increaseinrotor RPM associated with? 1An increaseinairflowthroughtherotorsystem. 2A decrease in airflow through the rotor system. 3A decrease in airspeed.

r,:.33 4 3 5456. What causes Coriolis effect? 5465. What Is the result of loading a helicopter so that the 1Differentlal thrust of rotor blades. CG is aft of the rearward limit? 2Changing angle of attack of blades during rotation. 1Insufficient aftcyclic control to decelerate propeny 3Shift in center of mass of flapping blade. during an approach. 2Inability of the pilot to recognize this dangerous condition 5457. Why are the rotor blades more efficient when when hovering in a strong headwind. operating in ground effect? 3Insufficient forward cyclic control toflyin the upper 1Induced drag is reduced. allowable airspeed range. 2Induced angle of attack is Increased. 5466. How is helicopter climb performance most adversely 3--Downwash velocity is accelerated. affected?

5458. What result does a level turn have on the total lift 1Higher-than-standard temperature and high relative hu- force and load factor? midity. 1Uft force remains constant and the load factor in- 2Lower-than-standard temperature and high relative hu- creases. midity. 2Lift force increases and the load factor decreases. 3Higher-than-standard temperature and low relative hu- 3Both total lift force and load factor increase. midity.

5459. What causes a helicopter to turn? 5467. Haw does high density altitudeaffect helicopter performance? 1Centrifugal force. 2Horizontal component of lift. 1Engine and rotor efficiency is Increased. 3Greater angle of attack of rotor blades on upward side of 2Engine and rotor efficiency is reduced. the rotor disc. 3Engine efficiency is reduced, but rotor efficiencyis Increased. 5460. What is the primary purpose of the tail rotor system? 5468. What type frequency vibrationis indicative of a 1 Maintain heading during forward flight defective tall rotor system? 2Act as a ruddertoassistincoordinatedturns. 3Counteract the torque effect of the main rotor. 1Low frequency. 2Medium frequency. 5481. Under what condition would it be necessary tocause 3High frequency. the tall rotor to direct thrust to the left on an American-made helicopter? 5469. What type frequency vibration is associated with the main rotor system? 1To maintain heading with a left crosswind. PTo counteract the drag of the transmission during 1Low frequency. autorotation. 2Medium frequency. 3To execute hovering turns to the right 3High frequency.

5482. What is the primary purpose of the free-wheeling 5470. What type frequency vibration is associated with a unit? defective transmission?

1To provide speed reduction between the engine, main 1Low frequency. rotor system, and tail rotor system. 2Medium frequency. 2To provide disengagement of the engine from the rotor 3High frequency. system for autorotation purposes. 5471. Which Is a major warning of approaching retreating 3To transmit engine power to the main' rotor, tail rotor, blade stall? generatorialtematnr, and other ac cessoriet 1High frequency vibration. 5463. The main rotor blades of a fully articuNted rotor 2Tendency to roll opposite the stalled side of the rotor. system can 3Pitchup of the nose. 1flap, drag, and feather collectively. 2flap, drag, and feather Independently of each other. 5472. What corrective action can c pilot take to prevent a 3flap and drag individually, but can only feather collec- retreating blade stall at its onset? tively. 1Reduce collective pitch and increase rotor RPM. 2Increase collectivepitchandIncreaserotor RPM. 5464. The main rotor blades of a semi-rigid system can 3Reduce collectivepitchand decreaserotor RPM. 1flap and feather as a unit. 2flap, drag, and feather Independently. 3flap and drag Individually, but can only feather collectively.

3444 5473. Which type rotor system is more susceptible to 5482. Within what Mach range does transonic flight regimes ground resonance? usually occur? 1Fully articulated rotor system. 1.50 to .75 Mach. 2Semi-rigid rotor system. 2.75 to 1.20 Mach. 3Rigid rotor system. 3-1.20 to 2.50 ME.ch.

5474. What corrective action can a pilot take to recover 5483. What is the highest speed possible without super- from settling with power? sonic flow over the wing?

1Increase forward speed and raisecollectivepitch. 1Initial buffet speed. 2Decrease forward speed and partially raise collective 2Critical Mach number. Pitch. 3Transonic index. 3Increase forward speed and partially lower collective Pitch. 5484. Whatisthefreestream Mach number which produces first evidence of local sonic flow? 6475. What limits the high airspeed potential of a helicopter? 1Supersonic Mach number. 2Transonic Mach number. 1--Ham tonic resonance. 3Critical Mach number. 2Retreating blade stall. s- -Rotor RPM limitations. 5485. At what Mach range does the subsonic flight range normally occur? 5478. How does VNi speed vary with altitude? 1Below .75 h iach. 1 Varies directly with altitude. 2From .75 to 1.20 Mach. 2Remains the same at all altitudes. 3From 1.20 to 2.50 Mach. 3Varies inversely with altitude. 5486. What is the principal advantage of a sweepback 5477. How should a quick stop be initiated? design wing over a straightwing design? 1Raise collective pitch. 1The critical Mach number willincrease significantly. 2Apply aft cyclic. 2Sweepback will increase changes in the magnitude of 3Decrease RPM while raising collective pitch. force coefficients due to compressibility. 3Sweepback will accelerate the onset of compressibility 5478. How should thepilotexecute apinnacle-type effect approach to a rooftop heliport in conditions of high wind and turbulence? 5487. What is the result of a shock-induced separation of airflow occurring symmetrically nes the wing root of a 1Steeper than normal approach, maintaining the desired sweptwing aircraft? angle of descent with collective. 2Normal approach, maintaining a slower-than-normal rate 1A high-speed stall and sudden pitchup. of descent with cyclic. 2A severe moment or "tuck under." 3Shallow approach, maintaining a constant line of descent 3Sevore porpoising. with cyclic. 5488. What is one disadvantage of a sweptwing design? 5479. The primary purpose of high-lift devices is to increase the 1The wing root stallspriortothe wingtipsection. 2The wingtipsectionstallspriortothe wingroot. 1VD_ 3Severe pitch down moment when the center of pressure 2lift at low speeds. shifts forward. 3drag and reduce airspeed. 5489. What is the condition known as when gusts cause a 5410. What is the primary function of the leading edge flaps sweptwing-type airplane to roll in one direction while yawing In landing configuration during the flare before touchdown? in the other? 1Prevent flow separation. 1Porpoise. 2Decrease rate of sink. 2 Wingover. 3Increase profile drag. 3Dutch roll. 5411. What effect does the leading edge slot in the wing 5490. What is the movement of the center of pressure have on performance? when the wingtips of a sweptwing airplane are shock-stalled first? 1Decrease profile drag. 2-- Charges the stalling angle of attack t.., a higher angle. 1Inward and aft. 3 Decelerates the upper surface boundary layerair. 2Inward and forward. 3Outward and forward.

35 t., 4 5

--- 5491. What is critical Mach number? 5500. (Refer to figures 1, 2, and 5.) What is the total fuel requi.ed at .78 Mach? 1-The highest flight speed possible without supersonic flow. 1-15,620 pounds. 2-The speed at which the fonvard shift of center of 2-16,820 pounds. pressure causes a severe pitch down. 3- 17,250 pounds. 3-The speed at which tho airflow over the wing first reaches the speed of sound. 5501. (Refer to figures 1, 2, and 5.) What is the ETE at .82 Mach? 5492. What equipment on a sweptwing airplane contributes to the control of a dutch roll? 1-43 minutes. 2-45 minutes. 1-Rudder lock. 3-47 minutes. 2-Yaw damper. 3-Rudder trim. 5502. (Refer to figures 1, 2, and 5.) What is the total fuel required at .82 Mach? 5495. Aircraft equipped with both high-speed and low- speed ailerons will use the outboard ailerons only during 1-15,434 pounds. 2-15,484 pounds. 1-low-speed operations. 3- 18,750 pounds. 2-high-speed operations. 3-tow-altitude operations. 5503. (Refer to figures 1, 2, and 5.) What approximate indicated Mach should be maintained to arrive over the BLH 5494. (Refer to figures 1, 2, and 5.) What is the ETE at VORTAC 8 minutes after passing TRM VORTAC? .80 Mach? 1-.84 Mach. 1-43 minutes. 2-.85 Mach. 2-45 minutes. 3-.86 Mach. 3-47 minutes. 5504. (Refer to figures 1, 2, and 5.) What is the specific 5495. (Refer to figures 1, 2, and 5.) What is the total fuel range in nautical miles per 1,000 pounds of fuel from level- required at .80 Mach? off to the SALOM Intersection using .78 Mach? 1-9,700 pounds. 1-42 NAM/1,000 pounds. 2-15,550 pounds. 2-43 NAM/1,000 pounds. 3-18,750 pounds. 3-44 NAM/1,000 pounds.

5496. (Refer to figures 1,2, and 5.) What approximate 5505. (Refer to figures 1 and 2.) immediately after takeoff indicated Mach should be maintained to arrive over the BLH on Rwy 25, communications fail. What action should the VORTAC 9 minutes after passing TRM VORTAC? pilot take?

1-.73 Mach. 1-Abort the departure and return to the airport. 2-.74 Mach. 2-Continue the flight according to the clearance. 3-.75 Mach. 3-Continue to the nearest suitableairport and land.

5497. (Refertofigures 1 and 5.) What approximate 5508. (Refer to figures 1 and 2.) Define the departure route Indicated Mach should be maintained to arriveover the from a takeoff on Rwy 25 to the en route phase according SALOM Intersection 5 minutes after passing BLH VORTAC? to the flight plan.

1-.85 Mach. 1-Direct VTU VORTAC, then via VTU R-114 to FLIPR INT., 2-.88 Mach. via SLI R-220 to SLI, via SLI R-080 to CHANGEOVER 3-.87 Mach. PT., via V64 TRM. 2 -Rwy heading to VTU VORTAC, then via VTU R-114 to 5495. (Refer to figures 1 and 5.) What is the specificrange FLIPR INT., via 066 BRN from MAAGG LMM to intercept in nautical miles per1,000 pounds of fuel from TRM and rnaini 'tin V64 to TRM VORTAC. VORTAC to the SALOM Intersection using .76 Mach? 3-Rwy h. wing to LAX VORTAC, turn left hewing 220° to 1-42 NAM/1,000 pounds. intercept VTU R-114 to FLIPR INT., via 066 BRN to 2-43 NAM/1,000 pounds. MAAGG LMM, via 060 BRN from MAAGG LtiM to 3-44 NAM/1,000 pounds. intercept and maintain V64 to TRM VORTAC.

8491. (Refer to figures 1, 2, and 5.) What is the ETE at 5607. (Refer to figures 1 and 2.) Wnat frequency should be .78 Mach? monitored during departure from LAX? 1-48 minutes. 1-125.2 or 385.4 MHz. 2-48 minutes. 2-120.95 or 379.1 MHz. 3-50 minutes. 3-124.3 MHz.

36 46 5508. (Refer to figure3.)During the snivel phase at 5518. (Refer to figure 3.) What instrument approach light Phoenix Sky Harbor Intl, what radio frequency will provide system, f any, is available for the LOC BC RWY 26L weather and airport conditions? approach at Phoenix Sky Harbor Intl.? 1-121.2 MHz. 1-None. 2-122.0 MHz. 2 -HIRL 3-124.1 MHz. 3-REIL.

5509. (Refer to figure 4.) The minimum weather condition to 5517. (Refer to figure 3.) Identify the final approach fix on clear a fNght for the POWER PLANT VISUAL RWY 26L the LOC BC RWY 26L approach at Phoenix Sky Harbor Intl. approach is 1-Upon Intercepting the glide slope beyond 1-PHX 5 DME. 1-1,000/3. 2-When crossing I-PHX 5 DME at 3,000 feet 2-4,000/3. 3-When crossing the SRP VORTAC on the glide slope. 3-4,000/8. 5515. (Refer to figure 3.) The touchdown zone elevation of 5510. (Refer to figure 4.) What are the minimum conditions the LOC BC RWY 26L approacn at Phoenix Sky Harbor Intl. for the base leg for the POWER PLANT VISUAL RWY 26L is approach? 1-1,132 feet 1-4,000 feet and remain on or east of the SRP R-170. 2-1,122 feet. 2-3,100 feet and remain on or west of the SRP R-170. 3-1,121 feet. 3-3,100 feet and remain on or east of the SRP R-170. 5519. (Refer to figure 3.) When should the pilot expect 5511. (Refer to figure 4.) The POWER PLANT VISUAL radar vectors to the final approach course of the LOC BC RWY 26L approach normally begins RWY 26L approach at Phoenix Sky Harbor Intl.? 1-15 flying miles from the airport 1--SALOM INT. 2-opposite South Mountain. 2 -ARLIN INT. 3-at ARLIN INT. 3-Approximately 25 NM from SRP VORTAC.

5512. (Refer to to figure 4.) ATC may clear the flight for the 5520. (Refer to figure 3.) Determine the FAR Part 121 POWER PLANT VISUAL RWY 26L only in radar environ- landing minimums for the LOC BC RWY 26L approach at ment and only Phoenix Sky Harbor Intl. 1-if the pilot agrees to cancel the IFR flight plan and PIC time 94 hours proceed VFR. Airplane V, maximum 2-after the pilot reports citing a charted landmark or a certificated weight 105 knots preceding aircraft. Vup approach speed 140 knots 3-If the approach is requested by the pilot. DME NOTAMed OTS 5513. (Refer to figure 4.) Why are charted visual flight 1-1,800/2. procedures, such as the POWER PLANT VISUAL RWY 26L, 2-1,900/2-1/4. established? 3-1,900/2-1/2. 1-For noise abatement purposes at locations with .1 5521. (Refer to figure 3.) Determine the FAR Part 135 operations. landing minimums for turbine powered aircraft on the LOC 2-To sequence landing aircraft and enable IFR approaches BC RWY 26L approach at Phoenix Sky HarborIntl. to have priority. PIC time 98 hours 3-To allow pilots to request the VFR approaches in lieu of Airplane Vso maximum IFR approaches. certificated weight 103 knots 126 knots 5514. (Refer to figure3.)Straight in minimums for a VI:, approach speed Category B aircraft equipped with DME on the LOC RC DME NOTAMed OTS RWY 26L approach are 1-1,800/2. 1-1,800/1. 2-1,900/2-1/4. 2-700/1. 3-1,900/2-1/2. 3-1,540/1. 5522. (Refer to figure 3.) What is the HAT a Category B 5515. (Refer to figure 3.) How is course reversal accom- aircraft may descend to if the pilot has Identified HADEN plished when outbound on the LOC BC RWY 26L approach INT on the LOC BC RWY 26L approach at Phoenix Sky at Phoenix Sky Harbor Intl.? Harbor Intl.? 1-Radar vector only. 1-418 feet. 2-Procedure turn beyond 10 NM. 2-500 feet 3-Holding pattern entry beyond 10 NM. 3-670 feet.

37 47 5523. (Refer to figures 6 and 7.) If communicationsare lost 5531. (Refer to figures 5, 6, 7, and 8.) Determine the ETE soon after takeoff on Rwy 11R at Tucson Intl., what altitude for the flight from TucsonIntl.to Los AngelesIntl. restrictions apply? 1-2 hours 10 minutes. 1-Maintain 17,000 feet to GBN, then climbto assigned 2-2 hours 15 minutes. altitude. 3-2 hours 19 minutes. 2-Climb in holding pattern (NW, rightturn, 128 inbound) to 9,000, then on course to 17,000 feetor lower assigned 5532. (Refer to figures 5, 6, 7, and 8.) Estimate the total altitude. fuel required (including missed approach) from Tucson Intl. 3-Remain at or below 9,000 feet to ROSKRINT, then to Los Angeles Intl. climb to and maintain 17,000 feet to GBN. 1-2,048 pounds. 5524. (Refer to figure 7.) What are the takeoffminimums 2-2,098 pounds. for Rwy 11R at Tucson Intl.? 3-2,218 pounds.

1-1 SM. 5533. (Refer to figures 5 and 6.) What TAS would be 2-800/1. required to arrive at the start descent position 24 minutes 3-4,000/3. after passing TNP?

5525. (Refer to figure7.)Determine the DEP CON 1-248 knots. frequencyforthe TUS2.GBN SID aftertakeoff from 2-251 knots. Rwy 11R at Tucson Intl. 3-254 knots.

1-125.1 MHz. 5534. (Refer to figures 5 and 6.) What TAS would be 2-118.5 MHz. required to arrive at the intersection of J104 20 minutes 3-119.0 Mhz. after passing GBN?

5526. (Refer to figures 6 and 7.)Using an average 1-268 knots. groundspeed of 140 knots, what minimum indicatedrate of 2-269 knots. climb must be maintained to meet the requiredclimb rate 3-272 knots. (feetper NM) to9,000 as specified on the SID? 5535. (Refer to figures 2 and 8.) Which approach control 1-349 ft/min. frequency is indicated for the TPN.DOWNE2 Arrival with 2 -560 ft/min. LAX as the destination? 3-584 ft/min. 1-128.5 MHz. 5527. (Refer to figure 6.) What CAS shouldbe used to 2-124.9 MHz. maintain the fixed TAS at the proposed altitude? 3-124.5 MHz.

1-157 knots. 5536. (Refer to figure 9.) At what point does the flight enter 2-167 knots. the final approach phase of the ILS RWY 25L at LAX? 3-172 knots. 1-FUELR INT. 5528. (Refer to figure 7.) How can the pilotreceive the 2-HUNDA INT. latest NOTAM's for the TUS-LAX flight? 3-Intercept of glide slope.

1-Monitor ATIS on 123.8 MHz. 5537. (Refer to figure 9.) What is the DH for the ILS RWY 2-Contact the FSS on 1222 MHz. 25L at LAX If the pilot has cornpleZed the initial Category II 3-Request ADCUS on any FSSor Tower frequency. certification within the preceding 6 months?

5529. (Refer to figure 7.) What distance isavailable for 1-201 feet takeoff on Rwy 11R at Tucson Intl.? 2-251 feet. 3-301 feet. 1-7,000 feet 2-9,129 feet. 5538. (Refer to figure 9.) The radio altimeter indication for 3-10,994 feet the DH at the inner marker on the ILS RWY 25L approach at LAX is 5530. (Refer to figure 7.) What effecton the takeoff run can be expected on Rwy 11R at Tucson Intl.? 1-101. 2-111. 1-Takeoff length shortened to 6,986 feet bydisplaced 3-201. threshold. 2-Takeoff run shortened by 0.8 percentrunway slope to the SE. 3-Takeoff runwill be lengthened by the 0.6 percent upsiope of the runway.

3848 5639. (Refer to figure 9) The 7,000-foot marker at BASET 5544. (Refer to figures 10 and 11.) What is the ETE for the INT nn the ILS RWY 25L approach at LAX inthe IFR Helicopter flight from Baker Airport to LAX? 1 maximum altitude at BASET INT. 1-1 hour 33 minutes. 2minimum altitude at BASET INT. 2-1 hour 36 minutes. 3minimum altitude at BASET INT for pilots approved for 3-1 hour 39 minutes. the 151 DH. 5545. (Refer to figures 10 and 11.) What is the total fuel 5540. (Refer to figure 9.) If the glide slope indication is lost required for the IFR Helicopter flight from Baker Airport to upon passing HUNDA INT on the ILS RWY 25L approach LAX? at LAX, what action should the pilot take? 1-3,038 pounds. 1Continue the approach as an LOC and add 100 feet to 2-3,658 pounds. the DH. 3-3,703 pounds. 2Immediately start the missed approach direct to INISH INT. 5546. (Refer to figures 10 and 11.) What TAS would be 3Continue to the MAP and execute the missed approach required to arrive at POM VORTAC 52 minutes after as Indicated. passing DAG VORTAC? 1-114 knots. 5641. (Refer to figure 9.) What approach lights are available 2-117 knots. for the ILS RWY 25L approach at LAX? 3-120 knots. 1ALSF-2 with sequenced flashing lights. 2MALSR with a displayed threshold.' 5547. (Refer to figures 10 and 11.) What TAS would be 3HIRL and TDZ/CL required to arrive at POM VORTAC 1 hour after passing DAG VORTAC? 5642. (Refer to figures 8 and 9.) What is the function of 1-102 knots. "LR-075 LAX" depicted below FUELR INT and BASET INT 2-105 knots. on the plan view of ILS RWY 25L at LAX? 3-108 knots. 1Urnits off-course on the left side of the LOC. 2Replaces the edge of the LOC indication where it is 5548. (Refer to figure 11.) The changeover point on V394 unreliable. between DAG VORTAC and POM VORTAC is 3Lead inradialfor trandon to the LOC course. 1halfway. 2-38 DME miles from DAG VORTAC. 5543. (Refer to figure 9.) What Is the position of the aircraft 3-64 DME miles from DAG VORTAC. on the ILS RWY 25L approach at LAX? 5549. (Refer to figure 11.) The minimum crossing altitude at NAV 2 APLES INT southwest bound on V394 is 1-7,500 feet 2-9,100 feet. 3-11,500 feet

5550. (Refer to figure 11.) What is the minimum crossing attitude at POM VORTAC when southwest bound on V210? 1-10,700 feet 2-10,300 feet 3-5,300 feet 5551. (Refer to figure9.) How can DOWNE INT be identified? 1ILAX 15 DME. 2LAX VORTAC 15 DME. 3LAX VORTAC R-249 and SLI VORTAC R-327.

5552. (Refer to figure 2.) How should the IFR flight plan be closed upon landing at LAX? 1Right of course just past BASET INT inbound. 1Contact Hawthorne FSS on 123.6 MHz. 2Left of course approaching DOWNE INT inbound. 2Phone Hawthorne FSS on 644.1020. 3Left of course just past DOWNE INT inbound. 3LAX tower -III close it automatically.

39 4 9 566$. (Refer to figure 9.) What tower and ground control 5561. (Refer to figures 12 and 14.) What is the specific frequencies should a helicopter use when operating from range in nautical air miles per 1,000 pounds of fuel from the west to the heliport on the SE sideof LAX? ECK to start descent using .78 Mach?

TOWER GROUND CONTROL 1-53 NAM/1,000. 2-54 NAM/1,000. 1-119.8 MHz 121.75 MHL 3-55 NAM/1,000. 2-120.35 MHz 121.75 MHz. 3-119.8 MHz 121.85 MHz. 5562. (Refer to figures 12 and 14.) What is the ETE at .76 Mach? 5664. (Refer to figures 12, 13 and 14.) What is the ETE from Greater Buffalo Intl. to Chicago O'Hare Intl. using 1-1 hour 15 minutes. .80 Mach? 2-1 hour 17 minutes. 3-1 hour 19 minutes. 1-1 hour 11 minutes. 2-1 hour 15 minutes. 5563. (Refer to figures 12 and 14.) What is the total fuel 3-1 hour 17 minutes. required at .76 Mach?

6665. (Refer to figures 12, 13, and 14.) Determine the total 1-14,702 pounds. fuel required for the flight from Greater BuffaloIntl.to 2-15,036 pounds. Chicago O'Hare Intl. using .80 Mach. 3-15,729 pounds. 1-15,357 pounds. 5564. (Refer to figures 12 and 14.) What approximate 2-15,995 pounds. indicated Mach should be maintained to arrive at the start of 3-15,845 pounds. descent 34 minutes after passing ECK?

5554 (Refer to figures 12 and 14.) What approximate 1-.67 Mach. indicated Mach should be maintained to arrive at the start of 2 -.68 Mach. descent 28 minutes after passing ECK? 3-.69 Mach. 1-.85 Mach. 5565. (Refer to figures 12 and 14.) What is the specific 2-.88 Mach. range in nautical air miles per 1,000 pounds of fuel from 3-.83 Mach. ECK to start descent using .76 Mach?

5657. (Refer to figures 12 and 14.) What is the specific 1-51.9 NAM/1.000. range In nautical air miles per 1,000 pounds of fuel from 2-52.9 NAM/1,000. ECK to start descent using .80 Mach? 3-53.8 NAM/1,000. 1-55 NAM/1,000. 5566. (Refer to figures 12 and 14.) What is the lowest MEA 2-58 NAM/1,000. for the en route portion from BUF to OBK? 3-57 NAM/1,000. 1-10,000 feet. UK (Refer to figures 12 and 14.) What is the ETE at 2-12,000 feet .78 Mach? 3-FL180. 1-1 hour 12 minutes. 5567. tFiefer to figure 14 and chart legend.) Identify the 2-1 hour 14 minutes. ARTCC thre a letter idents and HA-EFAS frequency for 3-1 hour 18 minutes. Chicago.

6559. (Refer to figures 12 and 14.) What is the total fuel 1-ZAU, 135.525 MHz. required at .78 Mach? 2-ORD, 269.9 MHz. 3-0BK, 122.0 MHz. 1-14,902 pounds. 2-15,537 pounds. 5568. (Refer to figure 14 and chart legend.) For that portion 3-18,328 pounds. of the flight on HL547, night time begins at

WM. (Refer to figures 12 and 14.) What approximate 1-sunset. indicated Mach should be maintained to arrive at the start of 2-1/2 hour after sunset. decent 32 minutes after passing ECK? 3-1 hour after sunset 1-.72 Mach. 5589. (Refer to figures 14 and 17.) identify the LORAN-C 2-.73 Mach. coordinates for Greater Buffalo Intl. 3-.74 Mach. 1-116.4 BUF 286.9', 3.5 NM. 2-42'55'44"N - 78'38'48"W. 3-42'58'26"N - 78'43'57"W.

4050 5670. (Refer to figures 14 and 17.) Identify the RNAV 5578. (Refer to figure 17.) Which waypoint should be setup coordinates for Greater Buffalo Intl. on the RNAV receiver after identifying thefinal approach fix? 1 -116.4 BUF 286.9', 3.5 NM 2_42.56.4eN 78.38,481N. 1-CYUGA. 3-4215818"N 78'43'57"W. 2-MAP. 3-GANIS. 6671. (Refer to figures 14, 15, and 16.) What is the ETE from Chicago Midway Airport to Greater BuffaloIntl.? 5579. (Refer to figure17.) What is the procedure for initiating the missed approach on the RNAV RWY 32 1-2 hours 21 minutes. approach at BUF? 2-2 hours 25 minutes. 3-2 hours 28 minutes. 1-Select GANIS Waypoint and establish a direct course, climbing to 2,700 feet. 557.1. (Refer to figures 14, 15, and 16.) What are the fuel 2-Select and maintain R-302 of BUF VORTAC climbing to reqdrements from Chicago Midway Airport to Greater 2,700 feet Buffalo Intl.? 3-Establish and maintainR-286.9of BUF VORTAC climbing to 2,700 feet 1-483 pounds. 2-632 pounds. 5580. (Refer to figure 17.) What type entry is appropriate 3-689 pounds. for the missed approach holding pattern on the RNAV RWY 32 approach at BUF? 6673. (Refer to figures 14 and 15.) What TAS should be maintained to arrive over CRL VORTAC 50 minutes after 1-Parallel. level off? 2-Direct 3-Tear drop. 1-183 knots. 2-185 knots. 5581. (Refer to figure 18.) A VFR helicopter flight originates 3-187 knots. at the Pan Am Metroport near the United Nations Complex and is scheduled to JFK IMI. List the appropriate route. 5574. (Refer to figures 14, 15, and 16.) If communications are lost after takeoff on Rwy 13L at Chicago Midway, what 1-West bank of East River to E 34th St via RESERVOIR action should the pilot take? ROUTE to JFK Intl. 2-East bank of East River to E 34th St via RESERVOIR 1- -Circle and land at Chicago Midway. ROUTE to JFK Intl. 2-CNmb on runway heading to 2,000 feet until 6 DME 3-East bank of East River to Williamsburg Bridge via miles from Midway, then maintain 3,000 to 25 DME from WILLIAMSBURG and RESERVOIR ROUTES to JFK Intl. Midway. Climb to FL180 and intercept J148. 3-Climb on runway heading to 1,300 feet, at 4 DME turn 5582. (Refer to figure 18.) What is the vertical extent ofthe out then climb to 2,000 feet until 8 DME miles from TCA along the route from Pan Am Metroport to JFK Intl.? Midway. Climb to and maintain 3,000 feet to 25 DME from Midway, then turn and climb to R.180 direct to 1-1,500 to 7,000 feet. SBN VORTAC. 2-1,700 to 7,000 feet 3-Surface to 7,000 feet 5575. (Refer to figure 14.) What type airway is HL547 used on the flight from Chicago Midway Airport to Greater Buffalo 5583. (Refer to figure 18.) What is the requested minimum Intl.? altitude on the CONEY ISLAND ROUTE from Flatbush Ave. to the boundary of JFK Intl.? 1-Non-jet High Level Route. 2-Helicopter Preferred Route. 1-1,700 feet MSL 3-Canadian High Level Airway. 2-2,000 feet AGL. 3-300 feet AGL 5578. (Refer to figure 14.) The VOR changeover point between SBN VORTAC and CRL VORTAC on J554 should 5584. (Refer to figure 18.) Under what condition, if any, may Special VFR be a helicopter flight depart JFK Intl. on a Clearance? 1-BENJO INT. 2-Halfway. 1-None. 3-ARTCC boundary. 2-Both pilot and helicopter are IFR certificated. 3-Clearance from JFK Intl. 5577. (Refer to figure 17.) How can the FAF on the RNAV RWY 32 approach at BUF be identified? 5585. (Refertofigure18.)Helicoptersen routeto LaGuardia below 1,400 feet should contact the tower on 1-The RNAV receiver will Indicate 175.1' and 2.5 DME miles from BUF VORTAC. 1-118.7 MHz. 2-The RNAV receiver will indicate a change from TO to 2-122.95 MHz. FROM and 0 deflection of the course needle. 3-128.05 MHz. 3-Two flashes/second on the OM beacon light 41 51 5585. (Refer to figure 18.) What frequency should helicop- 5595. (Refer to figures 21 and 23.) How should the pilot ters monitor when maintaining the HUDSC" RIVER ROUTE identify the position to leave V369 for the BILEE CUGAR4 outside the TCA? ARRIVAL?

1-123.06 MHz. 1-Intercept R-305 of IAH. 2-123.76 MHz. 2-21 DME miles from TNV. 3-122.9 MHz. 3-141 DME miles from DFW.

5587. (Refer to figures 19, 20, 21, and 23.) What is the ETE 5596. (Refer to figure 22 and 23.) In addition to VOR and from DFW Intl. to landing at IAH? DME, what electronicequipmentisrequiredforthe 1-54 minutes. VOR/DME RWY 32R approach at IAH? 2-58 minutes. 1-Altitude alerting system. 3-58 minutes. 2-Standby VOR and DME receivers. 3-VHF communications and transponder equipment 55118. (Refer to figures 19, 20, 21, and 23.) What is the total fuel required from DFW Intl. to landing at IAH? 5597. (Refer to figure 23.) The BILEE.CUGAR4 arrival ends 1-1,205 pounds. 1-at BANTY INT. 2-1,284 pounds. 2-at IAH VORTAC. 3-1,393 pounds. 3-when cleared to land.

5589. (Refer to figure 19.) Determine the TAS required to 5598. (Refer to figure 23.) What action should the pilot take arrive at CUGAR, 31 minutes after level-off. if communications were lost during the BILEE.CUGAR4 1-242 knots. arrival? 2-248 knots. 1-Proceed direct to IAH VORTAC, then outbound on the 3-249 knots. IAH R-125 for a procedure turn for final approach. 2-From BANTY INT, proceed to the IAF on the IAH 6690. (Refer to figure 19.) Determine the TAS required to then continue on the IAH 10 DME Arc to final approach. arrive at CUGAR, 29 minutes after level-off. 3-Proceed direct to IAH VORTAC, then to either IAF or the 1-281 knots. IAH 10 DME Arc to final approach. 2-288 knots. 3-291 knots. 5599. (Refer to figure 23.) Which approach lightingis available for Rwy 32R? 5591. (Refer to figures 20 and 22.) Which frequency should 1-MALSR with RAIL be selected to check airport conditions and weather prior to 2-HIRL departure at DFW Intl.? 3-TDZ and CL 1-117.0 MHz. 2-134.9 MHz. 5600. (Refer tofigure23.) Whet effect onproach 3-136.5 MHz. minimums, if any, does an inoperative MALSR for an aircraft with an approach speed of 120 knots at IAH? 5692. (Refer to figures 20, 21, and 22.) The frequency 1-None. change from departure control to ARTCC after departing 2-Increases RVR to 5,000 feet. DFW Intl. for IAH is 3-Increases RVR to 8,000 feet 1-135.5 to 128.0 MHz. 2-118.55 to 127.95 MHz. 5801. (Refer to figure 23.) Under what condition may a pilot 3-127.75 to 127.95 MHz. make a procedure turn while executing the VOR/DME RWY 32R approach at IAH? 5693. (Refer to figure 21.) Where is the VOR changeover 1-Only when cleared by ATC. point on V369 between DFW Intl. and TNV? 2-If not DME equipped. 1-Ft Worth/Houston ARTCC boundary. 3-When approaching IAH from GOMER INT. 2-81 NM from DFW Intl. 3-TORNN Intl. 5802. (Refer to figure 23.) While arcing left on the IAH 10 DME Arc, the pilot experiences a left crosswind component 5594. (Refer to figure 21 or 22.) What is the magnetic Where should the bearing pointer be referenced relative to variation at both DFW Intl. and IAH? the wingtippositiontomaintainthe10 DME range? 1-08 E. 1-On the left wingtip reference. 2-0. 2- Behind the left wingtip reference. 3-08 W. 3-Ahead of the left wingtip reference.

42 52 5003. Where should the RMI bearing pointer be located 5610. (Refer to figure 23.) What is the position of this flight relative to the wingtip reference to maintain a constant DME on the VOR/DME RWY 32R approach at Houston? distance in a left -hand arc with a right crosswind component? NAV - 1 1-On the left wingtip reference. FIEQ N. M. KNOTS MIN 2-Behind the left wingtip reference. 3-Ahead of the left wingtip reference. 116.610.2 6 // 5604. (Refer to figure 23.) When is the earliest time the pilot may initiate a descent from 460 feet MSL to land at IAH? 1-Anytime after GALES INT if the runway environment is visible. 2-Only after the IAH 1.3 DME if the runway environment is visible. 3-Only after the IAH 1 DME if the runway environment is visible.

5605. (Refer to figure 23.) How should the pilot identify the MAP on the IAH VOR/DME RWY 32R?

1-After time has elapsed from FAF. 2-IAH 1.3 DME. 3-IAH 1 DME. 1-On missed approach14.8 NM from GOMER INT. 5606. (Refer to figure 23.) At what point may the missed 2-Outside the 10 DME arc approaching R-125. approach be initiated on the VOR/DME RWY 32R approach 3-At the IAF on R-061. at IAF? 6611. (Refer to figure 25.) What is the maximum approach 1-Anytime after the FAF. speed for the COPTER VOR/DME 117' approach? 2-IAH 1.3 DME. 1-60 knots. 3-IAH 1 DME. 2-90 knots. 5607. (Refer to figures 20, 21, 23, and 24.) What is the ETE 3-91 knots. from DFW to landing at IAH? 5612 (Refer to figure 25.) What type approach lights are 1-2 hours 05 minutes. availablefor the COPTER VOR/DME 117° approach? 2-2 hours 19 minutes. 1-REIL and MIRL only. 3-2 hours 22 minutes. 2-Nonstandard REIL only. 3-REIL and nonstandard VASI only. 5606. (Refer to figures 20, 21, 23, and 24.) What is the total fuel required for the flight from DFW to IAH? 5613. (Refer to figure 25.) What NOTAM's are available at 1-140 pounds. Houma-Terrebonne Airport? 2-270 pounds. 1-NOTAM D and L' 3-206 pounds. 2-NOTAM L only. 5609. (Refer to figures 20, 21, 23, and 24.) What TAS 3-NOTAM D only. should be maintained to arrive at BILEE.CUGAR4 initial 5614. (Refer to figure 25.) If the COPTER VOR/DME 117° point 1 hour 5 minutes after level-off? approach is executed at 0630 local standard time, what 1-138 knots. minimums must be observed? 2-143 knots. 3-146 knots. 1- 440/1/2. 2-580/1/2. 3-580/3/4.

5615. (Refer to figure 25.) What is the VASI approach slope angle for Rwy 12 at Houma-Terrebonne? 1-2.5'. 2-3.0% 3-3.5%

ee 53 5616. (Refer to figure 25.) Determine the position of this 5622. (Refer to figure 26.) What is the minimum altitude for flight on the COPTER VOR/DME 117' approach. Category D aircraft at the FAF for the S-18 LDA/DME-21 RWY 18 approach? 1-8,120 feet. 2-8,480 feet. 3-8,900 feet.

5623. (Refer to figure 26.) On which IFR Low Altitude Charts can Lake Tahoe be found? 1-L panel 2G and Helicopter 5A. 2-2 panel G and 5 panel A. 3-H-2G, L--^.G, and 5A.

5624. The threshold crossing height listed in figure 26 for the VASI on Rwy 18 is 1-6,254 feet MSL 2-6,367 feet MSL. 3-47 feet AGL 5625. (Refer to figure 26.) Approximately what rate of descent at 120 knots is necessary for the LDA/DME-2 RWY 18 approach at Lake Tahoe? 1-Approaching InF TIBBY. 2-Starting to turn from the 5 DME arc to final approach. 1-250 ft /min. 3-Approaching BOURG INT during the missed approach 2-500 ft /min. procedure. 3-600 ft /min.

5617. (Refer to figure 25.) What type entry is appropriate 5626. (Refer to figure 26.) How can a pilot activate the forthe missed approachholdingpatternat Houma- approach lights to medium intensity at Lake Tahoe when Terrebonne? the tower is closed? 1-Direct only. 1-Contact the FSS on CTAF frequency. 2-Parallel or teardrop. 2-Key themikethree times on Unicorn frequency. 3-Teardrop only. 3-Key the mike five times on CTAF frequency.

5616. (Refer to figure 25.) At what point may the missed 5627. (Refer to figure 26.) What is the position of this flight approach be initiated? on the missed approach holding pattern at Lake Tahoe? 1-TBD 10.2 DME. 2-Upon expiration of time from FAF. NAV - 1 3-Anytime after FAF. L108.9iN. N. 11111111 MINI

5619. (Refer to figure 26.) What is the distance from the 11.580 8.IEI4 IAF to KINGS INT for the LDA/DME-2 RWY 18 approach? 1-19 DME miles. 2-20.4 DME miles. 3-21.3 DME miles.

5620. (Refer to figure 26.) Why is the localizer. South Lake Tahoe designated as LDA/DME? 1-DME is substituted for an outer marker. 2-The localizer is not aligned with the runway and all fixes are DME. 3-The localizer is wider than the standard ILS LOC and all fixes are DME.

5621. (Refer tofigure26.) What approach lightingis available for the LDA/DME-2 RWY 18 approach? 1-MIRL. 1-Turning from outbound leg. 2-MIRL and 2-light VASI. 2-Off course to the right inbound. 3-MALSF with sequenced flashing lights and 2-box VASI. 3-Turning on to the outbound leg.

'54 UK (Refer to figure 27.) From whom can a pilot request a 5636. (Refer to figure 28.) Determine the minimum weather OF steer in the Salisbury area? nditions for a Category D aircraft on the MLS RWY 19L 1-Salisbury FSS. -oach that must be forecast to avoid listing an alternate 2-Leesburg MS. on an IFR flight plan. 3-Patuxent Approach Control. 3. !!!S. (Refer to figure 27.) Why isthere an apparen 4. difference In course direction on the plan view of the LOC BC RWY 14 approach? 5b.... What are the azimuth limits on the MLS such as the one depicted in figure 28? 1-The localize, bends. 2-To adjust for the nearby obstacles. 1-5' each side of the centerline. 3-136' is the LOC course and 134' is a radial of SBY. 2-10' each side of the centerline. 3-40' each side of the centerline. 5430. (Refer to figure 27.) When may the missed approach at SBY be Initiated If the aircraft is equipped with DME? 5638. (Refer to figure 28.) What is the threshold crossing 1-Anytime after SBY 3 DME. height established by the VASI on Rwy 19L at ICT? 2-When time has expired from the FAF. 1-47 feet. 3-Anytime after reaching the MDA. 2-52-1/2 feet. 3-55 feet. 5631. (Reit" to figure 27.) What type VASI is installed for Rwy 14 at SBY? 5639. (Refer to figure 28.) Of what use is the back azimuth of the MLS at ICT? 1-4-1Ight VASI. 2-4-box VASI - 2 each side of runway. 1-Lateral guidance for the missed approach. 3-4-box VASI - all on left side of runway. 2-Backup system to replace front course failure. 3-Support for the DME/P system. 5132. (Refer to figure 27.) What is the purpose of the holding pattern at HEBRO INT on the LOC BC RWY 14 5840. (Refer to figure 28.) If 120 knots is maintained on the approach at SBY? final approach of MLS RWY 19L, what rate of descent will maintain the glide slope? 1-Timed approaches and course reversals. 2-En route and approach delays. 1-600 ft/min. 3-Climb or descent corridor and approach delays. 2-635 ft/min. 3-675 ft/min. 5633. (Refer to figure 27.) What type facility is WATERLOO as depicted on the plan view of the LOC BC RWY 14 5641. (Refer to figure 28.) Identify the FAF on the MLS approach at SBY? RWY 19L approach at ICT.

1-VOR. 1-M-JOZ 7.1 DME at 3,207 feet. 2-VOR/DME. 2-Interception of glidepath at 3,300 feet 3-TACAN. 3-Interception of glidepath at any point. 5634. (Refer to figure 27.) This flight is destined for the LOC BC RWY 14 approach at SBY. What minimum weather conditions'mist be forecast to avoid listing an alternate airport on the flight plan? 1-600/2-1/4. 2-1,000/3. 3-1,940/3-1/2.

5635. (Refer to figure 27.) What approach control facility, if any,is available when the tower isclosed at SBY? 1-None. 2-Patuxent Approach Control. 3-Washington Center Approach Control.

46 55 5642. (Refer to figure 28.) What Is the position of thisflight 5647. (Refer to figure 29.) What are the landing minimums on the MLS RWY 19L approach at CT? for a Category C aircraft on a straight-in NDB RWY 15 approach at CHS ifthe touchdown zone lights and NAV - 1 centerline lighting are inoperative? CHAN N. N. KNITS MIN 1-480/40. 5567.4 1123.9 2-480/50. 3-530/80.

5646. (Refer to figure 29.) Determine the position of this flight on the NDB RWY 15 approach according to the indications of the RMI.

1-Turning inbound on themissed approach holding pattern. 2-On entry to the missed approach holdingpattern. 3-Outbound on procedure turn.

5643. (Refer to figure 29.) This flight is destined forthe NDB RWY 15 approach at CHS. What minimumweather conditions must be forecast to avoid listingan alternate airport on an IFR flight plan?

1-1,000/3. 1-Inbound on the procedure turn. 2-1,980/3. 2-Left of course approaching the airport. 3-2,040/3. 3-On missed approach turning to intercept CHS R-055.

5644. (Refer tofigure29.) What minimum navigation 5649. (Refer to figure 29.) If the aircraft approaches on final equipment is necessary for the NDB RWY 15 approachat at 110 knots, what will be the time from FAF to MAP on the CHS? NDB RWY 15 approach at CHS? 1-ADF. 1-2 hours 27 minutes. 2-ADF and VOR. 2-2 hours 30 minutes. 3-ADF, VOR, and DME. 3-2 hours 37.5 minutes.

5645. (Refer to figure 29.) When may the pilotinitiate a 5650. (Refer to figure 30.) Identify the IAF(s) for the SDF missed approach on the NDB RWY 15 approachat CHS? RWY 31 approach at Reidsville. 1- Anytime atter the FAF. 1-KLUTE INT. 2-1" the CHS 2.5 DME. 2-Slammer NDB. 3-At expiration of time after FAF. 3-Greensboro VORTAC,MartinsvilleVOR/DME, and Danville VOR. 5646. (Refer to figure 29.) At what pointon the NDB RWY 15 approach at CHS may the pilot descendbelow the 5651. (Refertofigure30.) What minimum navigation MDA if the runway environment is in sight? equipment is necessary for the SDF RWY 31 approach at 1-Only after the CHS 2.5 DME. Reidsville? 2-Only after the time to MDA has expired. 1-VOR receiver. 3-Anytime after the FAF. 2-ILS receiver. 3-ILS and ADF receivers.

.5 646 11252. (Refer to figure 30.) What does the negative "L"on 5650. What information is provided by the MLS precision the plan view of the SOF RWY 31 represent? navigation system?

1The tower is on a UNICON frequency. 1Azimuth, elevation, and distance information. 2MIRL and VAST are activated by keying UNICOM 2Azimuth, elevation, end three-letter identification. froluimaY 3Range, elevation, and ISMLS readouts. 3Approach lighting on Rwy 13 and Rwy 31 are nonstandard. Mt Inaddition to basic Information, what expansion capabilities does the MLS have? 5653. (Refer to figure 30.) If the aircraft approaches on final at 115 knots, what will be tne the from FAF to MAP on the 1Back azimuth glide slope. SOF RWY 31 approach at Reidsville? 2Back azimuth and data transmissions. 3Variable front and back azimuth upon request. 1-2 hours 34 minutes. 2-2 hours 37 minutes. 5662. What azimuth coverage of the MLS can be ex- 3-2 hours 40 minutes. pected? 5054. (Refer to figure 30.) Why is the SDF RWY 31 1Laterally 20' each side, vertically 15' to 20,000 feet, and approach classified as SDF rather than LOC RWY 31? range 50 NM. 2Laterally 40' each side, vertically 15' to 20,000 feet, and 1There is no outer marker. range 20 NM. 2The procedure turn Is nonstandard. 3Laterally 15' each side, vertically 6' to 20,000 feet, and 3The localizer course Is wider than an ILS LOCcourse. range 20 NM.

5655. (Refer to figure 31.) What is the laming minimum for 5663. What is the difference, if any, between the front and a Category D aircraft for the ASR RAP' 16 approach at back azimuth of the MLS? Ashville Regional? 1None, except indicator reversal. 1-3,000-foot MDA. 2Transmissions are at a lower rate. 2-24/4 miles visibility. 3Back azimuth has no DME/P. 3-900-foot ceiling. 5664. In addition to navigation information, what data is WM (Refer to figure 31.) What are the Category C transmitted on the t " ,S frequencies? approach minimums for the ASR RWY S-8R approach at Atlanta/Fulton County Airport? 1MLS status, missed approach procedure, and airport conditions. 1-1,540/2. 2ATC clearances, missed approach procedures, and 2-1,590/2. airport conditions. 3-1,540/1-1/2. 3MLS status, airport conditions, and weather.

5657. (Refer to figure 31.) What are the ASR RWY 20L 5665. What does operational flexibility of the MLS system approach minimums for Category A aircraft at include? Allanta/Dekalb-Peachtree Airport with the MALSF inoperative and using the Fulton County-Brown Field altimeter 1Selectable glidepath angles and boundaries providing setting? obstruction clearance in the terminal area. 2An azimuth of 40' in width providing obstacle clearance 1-1,560/3/4. within 22 NM of the airport 2-1,560/1-1/4. 3Curved and segmented approaches collocated with a 3-1,610/1-1/4. fixed glkiepath angle.

5656. (Refer to figure 31.) What are the ASR RWY 20L 5668. LORAN-C Is based upon measurements of the approach minimums for Category C aircraft at difference in time arrival of pulses generated by what type Atianta/Dekalb-Peachtree with the MALSF Inoperative and radio stations? using the Fulton County-Brown Fieldaltimeter setting? 1A group of stations operating on the 108-115 MHz 1-1,520/1-1/2. frequency band. 2-1,560/1-1/2. 2Two stations opera$Mg on the 90-110 MHz frequency 3-1,560/2. band. 3A chain of stations operating on the 90-110 MHz 56511. (Refertofigure 31.)Determine ASR approach frequency band. minimums for Category C aircraft on F:Ny 8L at Atlanta/The William B. Hartsfield if the ALFS1 is inoperative. 1-1,480/40. 2-1,530/60. 3-1,480/60.

47 -.? 5 7 5667. For what service has LORAN-C been approved? 5675. Which component associated with the ILS is identi- fiedby the 1-1FR navigation in U.S. coastal areas and nonprecision last twolettersofthelocalizer group? approaches. 1Inner marker. 2VFR navigation in the 48 contiguous states and District 2Middle compass locator. of Columbia. 3Outer compass locator. 3IFR and VFR navigation in the 48 contiguous states and District of Columbia. 5676. Which component associated with the ILS is identified by the first two letters of the localizer idenLication 5668. What kindof network makes up the OMEGA group? Navigation System. 1Inner marker. 1Four basic navigation facilities having worldwide signal 2 Middle compass locator. coverage. 3Outer compass locator. 2Eight stations transmitting on four basicnavigation frequencies. 5677. What aural and visual indications should Ix''served 3Four basic navigation facilities transmitting on four basic over an ILS inner marker? navigation frequencies. 1Continuous dotsattherateofsixper second. 5669. When is an OMEGA station said to be operating in 2Continuous dashes at the rate of two per second. full format? 3Alternate dots and dashes at the rate of two per second.

1The station is transmitting on the basic frequencies plus 5678. What aural and visual indications should be observed the unique frequency. over an ILS middle marker? 2The station is transmitting on one of the four basic frequencies in the VLF range. 1Continuous dotsat therateofsixper second. 3The station is transmitting on eight VHF frequencies, 2Continuous dashes at the rate of two per second. plus four discreet frequencies. 3Alternate dots and dashes at the rate of two per second

5670. What Information does OMEGA provide? 5679. What aural and visual indications should be observed over an ILS outer marker? 1Uninterrupted azimuth guidance and tracking. 2 Fbdng information to an accuracy of plus or minus 2 NM. 1Continuous dotsattherateofsixper second. 3Guidance, tracking, and fixing information. 2Continuous dashes at the rate of two pa second. 3Alternate dots and dashes at the rate of two per second. 5671. Under what condition may OMEGA navigation be usedin the conterminous United States and Alaska? 5680. What ...... luency range does the localizer transmitter of the ILS operate within? 1The equipment is tested within the previous 30 days. 1- 108.10 to 118.10 MHz. 2The equipment is used in conjunction withan inertial 2-108.10 to 111.95 MHz. navigation system. 3All navigation equipment otherwise required by the FAA 3- 108.10 to 117.95 MHz. be installed and operating. 5681. What aurai and visual indications should be observed 5672. What type navigation system is Inertial Navigation over the ILS back course marker? System (INS)? A navigation computer whichprovides 1A series of two dot combinations. position 2Continuous dashes at the rate of one per second. 3A series of two dash combinabons. 1from information by compass, airspeed, andan input of wind and variation data 5682. The lowest ILS Category II minimums are 2from radar type sensors that measure ground speed and drift angles. 1DH 50 feet and RVR 1,200 feet. 3by signals from self-contained gyros and accelerometers. 2DH 100 feet and RVR 1,200 feet. 3DH 150 feet and RVR 1,500 feet 5673. WhatisaFlight Management System (FMS)? 5683. What is the lowest Category IIIA minimum? 1A computer system programmed to update position by reference to conventional navigation aids. 1DH 50 feet and RVR 1200 feet. 2A transponder type navigation system which receives 2RVR 1,000 feet. data for positions from satellites. 3RVR 700 feet 3A doppler radar system, computerized to provide position from groundspeed and variations of direction. 5684. How does the SDF differ from anILS LOC?

5674. What functions are provided by ILS? 1SDF 6' or 12' wide, ILS 36 to 6'. 2SDF offset from runway plus 3', ILS aligner! with 1Azimuth, distance, and vertical angle. runway. 2Azimuth, range, and vertical angle. 3SDF 15' usable off course indications, ILS 35'. 3Guidance, range, and visual information. 5 48 5695. How does the LDA differfrom anILS LOC? 5694. What are the indications of PAPI7 1LDA - ir or 126 wide, ILS - 3' to r. 1Highwhite, on glidepathred and white; lowred. 2LDA - offset from runway plus 3', ILS- aligned with 2Highwhite, on glidepathgreen; lowred. rumvay. 3Highwhite and green, on glidepathgreen; lowred. 3LOA 156 usable off course indications, ILS-356. 5695. What does the pulsating VASI consist of? MI6. What DME indications should a pilot observe when directly over a VORTAC site at 12,000 feet? 1Three-light system, two pulsing and one steady. 2Two-light projectors, one pulsing and one steady. 1-0 DME miles. 3One-light projector, pulsing (some steady for on course). 2-2 DME miles. 3-2.3 DME miles. 5696. What are the indications of the pulsating VASI7

5667. Where does the DME indicator have the greatest 1 Highpulsing white, on glidepathgreen; lowpulsing error between the ground distance and displayed distance red. to the VORTAC? 2HighpL ag white, on glidepathpulsing red and white or steady white; lowpulsing red. 1High &Utiles close to the VORTAC. 3Highpulsing white, on course and on glidepathsteady 2Low altitudes close to the VORTAC. white, off course but on glidepathpulsing white and 3Low altitudes far from the VORTAC. red; lowpulsing red.

5665. What does the tri-color VASI consist of? 5697. Whatisthe advantage of a three-barVASI7 1Three light bars; red, green, and amber. 1Pilots have a choice of glide angles. 2One light projector with three colors; red, green, and 2A normal glide angle is afforded both high and low amber. cockpit aircraft 3Three glide slopes, each a different color, red green, and 3The three -bar VASI is much more visible and can be amber. used at a greater height.

5669. Which color on a tri-color VASI is a "high" ine _ation7 5696. A pilot of a high-performance airplane should be 1Red. aware that flying a steeper- than - normal VASI glide slope 2Amber. angle may ream in 3. Green. 1a hard landing. 2 increased landing rollout. 5111.L. Which color on a tri-color VASI is an "on course" 3landing short of the runway threshold. indicatio 7 1Red. 5699. The higher glide slope of the three-bar VASI is 2Amber. intended for use by 3Green. 1high performance aircraft. 2helicopters. 5691. Which color on a tri-color VASI is a "low" indication? 3high cockpit aircraft. 1Red. 2 litter. 5700. What is the purpose of REIL7 2 .green. 1Identification of a runway surrounded by a preponder- ance of other lighting. 5692. What is the normal range of the tri-color VASI at 2Identification of the touchdown zone to prevent landing night? short. 1-5 miles. 3Establish visual descent guidance information during an 2-10 miles. approach. 3-15 miles. 5701. Identify REIL. 5693. What does the Precision Approach Path Indicator 1Amber lights for the first 2,000 feet of runway. (PAPI) consist of? 2Green lights at the threshold and red lights at far end of 1Row of four lights parallel to the runway; red, white, and runway. green. 3Synchronized flashing lights laterally at each side of the 2Row of four lights perpendicular .to the runway; red and runway threshold. whita. 3One light projector with two colors; red and white.

5 9 49 5702. .What is the advantage of HIRL or MIRL on an IFR 5709. What restriction applies to a large, turbine-powered rummy as compered to a VFR runway? airplane operating to or from a primary airport in a TCA? 1Lights are closer together and easily distinguished yrom 1Must not exceed 200 knots within the TCA. surroundthg fights. 2Must operate abows the floor *len within lateral limits of 2Amber lights replace white on the last 2,000 feet of the TCA. runway for a caution zone. 3Must operateinaccordancewithIFR procedures 3Alternate red and white lights replace the white on the regardless of weather conditions. last 3,000 feet of runway for a caution zone. 5710. What service is provided for aircraft operating within 5703. Identify touchdown zone lighting (TOIL). the outer area of an ARSA? 1Two rows of transverse light bars disposed symmetrically 1Th3 same as within the ARSA when communications about the runway centerline. and radar contact is established. 11Flush centerlinelights spacedat50-footintervals 2Radar vectors to and from secondary airports within the extending through the touchdown zone. outer area. 3Alternate white and green center line lights extending 3Basic radar service only when communications and radar from 75 feet from the threshold through the touchdown contact is established. IMO. 5711. What services are provided foraircraft operating 5704. Identify runway remaininglightingon centerline within the ARM? lighting systems. 1Sequencing of arriving aircraft,separation of aircraft 1Amber lightsfrom 3,000 feetto1,000 feet,then (except between VFR aircraft), and traffic advisories. alternate red and white lights to the end. 2Sequencing of arriving aircraft (except VFR aircraft), 2Alternate red and whitelights from 3,000 feetto separation between all aircraft, and traffic advisories. 1,000 feet, then red lights to the end. 3Sequencing of all arriving aircraft, separation between all 3Alternate red and white lights from 3,000 feet to the end aircraft, and traffic advisories. of the runway. 5712. What pilot certification and aircraft equipment are 5701 Identify taxi turnoff lights associated with the center- required for operating in an ARM? line lighting system. 1No specific certification but a two-way radio. 1Alternate blue and whitelightscurving fromthe 2At least a private pilot certificate and two-way radio. centerline of the runway to the centerline of the taxiway. 3At least a private pilot certificate, two-way radio, and a 2White lights curving from the centerline of the runway to TSO-C74b transponder. the centerline of the taxiway. 3Blue lights curving from the centerline of the runway to 5719. What hazards to aircraft and its occupants may exist the centerline of the taxiway. in restricted areas?

5701 How can a pilot identify a military airport at night? 1High speed military aircraft maneuvers. 2Invisible hazards such asartilleryfiringor guided 1Green, yellow, and white beacon light missiles. 2White and red beacon light with dual flash of the white. 3Classified military operations of a hazardous nature. 3Green and white beacon light with dual flash of the white. 5714. Why are certain areas classified as Warning Areas?

5707. How can a pilot identify a lighted heliport at night? 1Any hazards within may be avoided easily with good vigilance. 1Green, yellow, and white beacon light 2Hazardous operations are rare but inquiries should be 2White and red beacon light with dual flash of the white. made prior to entering the area 3Green and white beacon light with dual flash of the 3Invisible hazards exist in international airspace which white. cannot be controlled.

5701 Identify the runway distance remainingmarkers. 5715. What is the purpose of MOA's? 1Signs with increments of 1,000 feet distance remaining. 1To protect military aircraft operations from civil aircraft 2Red markers laterally placed across the runway at 2To separate military training activities from IFR traffic. 3,000 feet from the end. 3To separate military training activities from both IFR and 3Yellow marker laterally placed across the runway with VFR traffic. signs on the side denoting distance to end. 5716. Who is responsible forcollision avoidance in an MOA? 1Military controllers. 2ATC controllers. 3Each pilot. 5717. Which aeronautical chart depicts Military Training 5726. Under what situations are faster/larger helicopters Routes (MTh) above 1,500 fee? integrated with fixed-wing aircraft?

1IFR Low Altitude En Route Chart. 1IFR flights, noise avoidance routes, and use of runways 2IFR High Altitude En Route r'hart. or taxiways. 3IFR Planning Chart 2Use of taxiways, sequencing for takeoff and landing, and use of the same traffic patterns. 571$. Under what condition does ATC Issue Safety Alerts? 3Use of taxiways, sequencing for takeoff and landing, and 1When collision with another aircraft is imminent. use of the same loading ramps. 2If the aircraft altitude is noted to be in close proximity to 5727. Whatis a helicopterpilot's the surface or an obstacle. responsibility when cleared to "air taxi" on the airport? 3When weather conditions are extreme and wind shear or large hail is in the vicinity. 1Taxi directtodestinationasquickly as possible. 2Taxi at hover altitude using taxiways. 571$. What is the hijack code? 3Taxi below 100 feet AGL avoiding other aircraft and 1-7200. personnel. 2-75CO. 3-7777. 5728. What action is expected of an aircraft upon landing at a controlled airport?

5720. Which range of codes should a pilot avoid switching 1Continue taxiing in the landing direction until advised by through when changing transponder codes. the tower toswitchto ground controlfrequency. 1-0000 through 1000. 2Exit the runway at the nearest suitable taxiway and 2-7200 and 7500 series. remain on tower frequency until instructed otherwise. 3-7500, 7800, and 7700 series. 3Exit the runway at the nearest suitable taxiway and switch to ground cont. of upon crossing the taxiway 5721. To assure expeditious handling of a civilianair holding lines. ambulanceflight,the word "LIFEGUARD" should be entered In which section of the flight plan? 5729. What is the pilot's responsibility for clearance or instruction readback? 1Aircraft type /special equipment block. 2Pilot's name and address block. 1Except for SID's, read back altitude assignments, altitude 3Remarks block. restrictions, and vectors. 2If the clearanceorinstructionisunderstood, an 5722. What airport condition is reported by the tower when acknowledgment is sufficient. more than one wind condition at different positions on the 3Read back the entire clearance or instruction to confirm airport is reported? the message is understood.

1 Light and variable. 5730. Under what conditions may a pilot on an IFR flight 2Wind shear. plan comply with authorization to maintain "VFR on Top"? 3Frontal passage. 1Maintain IFR flight plan but comply with visual flight rules 5723. How should a pilot describe braking action? while in VFR conditions. 2Maintain VFR altitudes, cloud clearances, and comply 1-00 percent, 50 percent, 75 percent, or 100 percent. with applicable instrument flight rules. 2Zero-zero, fifty-fifty, or normal. 3Maintain IFRaltitudes, VFR cloud clearances, and 3Nil, poor, fair, or good. comply with applicable instrument flight rules.

5724. When "gate hold" procedures are in effect, what 5731. What cloud clearance must be complied with when action should the pilot take? authorized to maintain "VFR On Top"? 1Contact ground control prior tostarting engines for 1May maintain VFR clearance above, below, or between sequencing. layers. 2Taxi into position and hold prior to requesting clearance. 2Must maintain VFR clearance above or below. 3Start engines, perform pretakeoff check, and request 3May maintain VFR clearance above or below, but not clearance prior to leaving the parking area. between layers.

5725. What special consideration is given forturbine- 5732. In what areas will ATC not authorize "VFR On Top"? powered aircraft when "gate hold" procedures are in effect? 1ARSA's and TCA's. 1They are given preference for depaiture over other 2Continental Control Area. aircraft 3 P ;A's. 2They are expected to be ready for takeoff when they reach the runway or warmup block. 3They are expected to be ready for takeoff prior to taxi and will receive takeoff clearance prior to taxi.

51 61 5733. What separation or service by ATC isafforded pilots 5741. When a composite flight plan indicates IFR for the authorized "VFR On Top"? first portion of the flight, what is the procedure for the 1The same afforded all IFR flights. transition? 2-3 miles horizontally instead of 5. 1The IFR portion is automatically canceled and the VFR 3Traffic advisories only. portion is automatically activated when the pilot reports VFR conditions. 5734. When a speed adjustment is necessary to maintain 2The pilot should advise ATC to cancel the IFR portion separation, what minimum speedmay ATC request of a and contact the nearest FSS to activate the VFR portion. turbine-powered aircraft operating below 10,000 feet? 3The pilot should advise ATC to cancel the IFR portion 1-200 knots. and activate the VFR portion. 2-210 knots. 3-250 knots. 5742. Which IFR fixes) should be entered on a composite flight plan? 95. When a speed adjustment is necessary to maintain 1All compulsory reporting points en route. separation, what minimum speed may ATC request of a 2The VOR's that define the IFR portion of the flight turbine-powered aircraft departing an airport? 3The fix where the IFR portion is to be terminated. 1 -188 knots. 2-210 knots. 5743. When a composite flight plan indicates VFR for the 3-230 knots. first portion of the flight, what is the procedure for the transition? 5736. If ATC requests a speed adjustment that is not within 1The VFR portion is automatically canceled and the IFR the operating limits of the aircraft, what actionmust the pilot take? portion is automatically activated when the pilot reports IFR conditions. 1Maintain an airspeed within the operating limitationsas 2The pilot should advise ATC to cancel VFR and activate close to the requested speed as possible. the IFR portion of the flight 2Attempt to use the requested speedas long as possible, 3The pilot should close the VFR portion with the nearest then request a reasonable airspeed from ATC. FSS and request the IFR clearance at least 5 minutes 3Advise ATC of the airspeed that will be used. prior to IFR.

5737. What are FDC NOTAM's? 5744. What is the suggested time interval for filing and requesting an IFR flight plan? 1Conditions of facilities en route thatmay cause delays. 2Time critical aeronautical informationof a temporary 1File at least 30 minutes prior to departure and request nature from distant centers. the clearance not more than 10 minutes prior to taxi. 3Regulatory amendments to published IAP'sand charts 2File at least 30 minutes prior to departure and request not yet available in normally published charts. the clearance at least 10 minutes prior to taxi. 3File at least 1 hour prior to departure and request the 5735. What type information is disseminatedfrom NOTAM clearance at least 10 minutes prior to taxi. D's? 5745. How should the route of flight be defined on an IFR 1Status of navigation aids, ILS's, radar serviceavailable, flight plan? and other information essential to planning. 2Airport or primary runway closings,runway and taxiway 1A simplifiedrouteviaairways or jetrouteswith conditions, and airport lighting aids outages. transitions. 3Temporary flightrestrictions,changesinstatusin 2A route via airways or jet routes with VOR's and fixes navigational aids, and updateson equipment such as used. VASI. 3A route via airways orjetroutes withonlythe compulsory reporting points. 5739. What type information is disseminatedfrom NOTAM L's? 5746. How should an off-airway direct flight be definedon an IFR flight plan? 1Conditions of facilities en route thatmay cause delays. 2Airport or primary runway closings,runway and taxiway 1The initialfix,the true course, and thefinalfix. conditions, and airport lighting aids outages. 2All radio fixes over which the flight will pass. 3lime critical information ofa permanent nature that is 3The Mital fix, all radio fixes which the pilot wishes to be not yet available in normally published charts. compulsory reporting points, and the final fix.

5740. How often are NOTAM's broadcastto pilots on a scheduled basis?

1-15 minutes before and 15 minutes after thehour. 2Between weather broadcasts on the hour. 3Hourly, appended to the weather broadcast. 5747. How are RNAV routes defined on the IFR flight plan? 5754. On what performance is obstacle clearance based for IFR departures, including SID's? Cross end of runway 1Define each waypoint using degree-distance fixes based plus 35 feet AGL, on appropriate navigational aids or by latitude/longitude. 2List the initial and final fix with at least one waypoint 1then minimum climb of 150 feet per NM after takeoff. each 200 NM. 2climb to 400 feet prior to turn at the end of the runway, 3The initial and final fix must be an established radio fix, and then climb at least 200 feet per NM. then each waypoint in between is defined using degree- 3climb to 400 feet prior to turn at the end of the runway, distance fixes based on appropriate navigational aids. and then climb at least 150 feet per NM.

5748. What is one limitation when filing a random RNAV 5755. In what way are SID's depicted inplan view? route on an IFR flight plan? 1"Vectors" provided for navigational guidance or "Pilot 1The waypoints must be located within 200 NM of each NAV" with courses the pilot is responsible to follow. other. 2"Vectors" and "Pilot NAV" for pilots to use at their 2The entire route must be within radar environment. discretion. 3The waypoints may only be defined by degree-distance 3Combined textual and graphic form which are mandatory fixes based on appropriate navigational aids. routes and instructions.

5749. Under what condition may a pilot cancel an IFR flight 5756. What action should a pilot take if asked by ARTCC to plan prior to completing the flight? "VERIFY 9,000" and the flight is actually maintaining 8,000? 1Anytime it appears the clearance will cause a deviation 1Immediately climb to 9,000. from FAR. 2Report climbing to 9,000. 2Anytime within controlled airspace by contacting ARTCC. 3Report maintaining 8,000. 3Only ifin VFR conditionsinother than a PCA. 5757. Where are position reports required on an IFR flight 5750. What minimum information does an abbreviated on airways or routes? departure clearance "cleared as filed" include? 1Over all designated compulsory reporting points. 1Clearance limit and en route altitude. 2Only where specifically requested by ARTCC. 2Clearance limit, en route altitude, and SID, if appropriate. 3When requested to change altitude or advise of weather 3Destination airport, en route altitude, and SID, if appro- conditions. priate. 5758. Which reports are required when operating IFR in 5751. Under what condition does a pilot receive a "void radar environment? time" specified in the clearance? 1Position reports, vacating an altitude, unable to climb 1On an uncontrolled airport. 500 feet per minute, and time and altitude reaching a 2When "gate hold" procedures are in effect. holding fix or point to which cleared. 3If the clearance is received prior to starting engines. 2Position reports, vacating an altitude, unable to climb 500 feet per minute, time and altitude reaching a holding 5752. What is the normal procedure for IFR departures at fix or point to which cleared, and a change in average locations with pretaxi clearance programs? true airspeed exceeding 5 percent or 10 knots. 1Pilots request IFR clearance when ready to taxi. The 3Vacating an altitude,unable to climb 500 feet per pilot will receive taxi instruction with clearance. minute, time and altitude reaching a holding fix or point 2Pilots request IFR clearance when ready to taxi. Pilots to which cleared, a change in average true airspeed will receive taxi clearance, then receive IFR clearance exceeding 5 percent or 10 knots, and leaving any while taxiing or on runup. assigned holding fix or point. 3Pilots request IFR clearance 10 minutes or less prior to 5759. Which reports are always required when on an IFR taxi, then request taxi clearance from ground control. approach not in radar contact? 5753. What is the purpose of the term "hold for release" 1Leaving FAF inbound or outer marker inbound and when included in an IFR clearance? missed approach. 1A procedure for delaying departure for traffic volume, 2Leaving FAF inbound, leaving outer marker inbound or weather, or need to issue further instructions. outbound, and missed approach. 2When an IFR clearance is received by telephone, the 3Leaving FAF inbound, leaving outer marker inbound rr pilot will have time to prepare for takeoff prior to being outbound, procedure turn outbound and inbound, al .. released. visual contact with the runway. 3Gate hold procedures are in effect and the pilot receives an estimate of the time theflightwill be released.

6363 5760. What action should a pilot take if within 3minutes of 5768. What is the primary purpose of a STAR? a clearance limit and further clearance has not been rroeived? 1Provide separationbetween IFR and VFRtraffic. 2Simplify clearance delivery procedures. 1Assume lost communications and continueas planned. 3Decrease traffic congestion at certain airports. 2Plan to hold at cruising speed until further clearanceis received. 5769. When does ATC issue a STAR? 3Start a speed reduction to holding speed in preparation for holding. 1Only when ATC deems it appropriate. 2Only to high priority flights. 5761. What report should the pilot make ata clearance 3Only upon request of the pilot. limit? 5770. What action(s) should a pilot take if vectored across 1lime and altitude/flight level arrivingor leaving. thefinalapproach course duringanIFR approach? 2Time, altitude/flight level, and expected holding speed. 3lime, altitude /flight level, expected holding speed,and 1Continue on the last heading issued until otherwise inbound leg length. instructed. 2Contact approach control, and advise that the flight is 5762. Maximum holding speed for a propel;er-driven air- crossing the final approach course. plane is 3Turn onto final, and broadcast in the blind that the flight has proceeded on final. 1-156 knots. 2-175 knots. 5771. While being vectored to the final approach course of 3-210 knots. an IFR approach, when may the pilot descend to published altitudes? 5763. Maximum holding speed for a turbojet airplane above 14,000 feet is 1Anytime the flight is on a published leg of an approach chart. 1-210 knots. 2When the flight is within the 10-mile ring of a published 2-230 knots. approach. 3-265 knots. 3Only when Approach Control clears the flight for the approach. 5764. Maximum holding speed fora turbojetairplane between 6,000 and 14,000 feet is 5772 When ;. radar service terminated while vectored for 1-175 knots. an IFR approach at an uncontrolled airport? 2-200 knots. 1Only upon landing or advised to change to advisory 3-210 knots. frequency. 2When aligned on the final approach course. 5765. When using a flight director system, what rate of turn 3When cleared for the approach. or bank angle should a pilot observe during turns ina holding pattern? 5773. When cleared for an IFR approach to an uncontrolled airport with no FSS, what precaution should the pilot take 1 -3' per second or 25' bank, whichever isless. after being advised to change to 2-3' per second or 30' bank, whichever isless. advisory frequency? 3-1-112' per second or 25' bank, whicheveris less. 1Monitor ATC for traffic advisories as well as UNICOM. 2Broadcast intentions and continually update position 6766. When holding at an NDB, at what point should the reports on UNICOM. timing begin for the second leg outbound? 3Wait until visual contact Is made with the airport and 1Abeam the holding fix or when the wingsare level after broadcast intentions to land. completing the turn to the outbound heading, whichever occurs first 5774. Under what condition may a pilot file an IFR flight plan containing a special or privately owned IAP? 2At the end of a 1-minute standard rate turn afterstation Pang& 1Upon approval of ATC. 3When abeam the holding fix. 2Upon approval of the owner. 3Upon signing a waiver of responsibility. 5767. When entering a holding pattern above 14,000feet, the initial outbound leg should not exceed 5775. When may a pilot execute a missed approach during 1-1 minute. an ASR approach? 2-1-1/2 minutes. 1Anytime at the pilot'sdiscretion. 3-1-1/2 minutes or 10 NM, whichever is less. 2Only ai the MAP. 3Only when advised by the controller.

A4 5778. When simultaneous approaches are in progress, how 5783. What minimum condition is suggested for declaring does each pilot receive radar advisories? an emergency? 1-On tower frequency. 1-Anytime the pilot is doubtful of a condition that could 2-On approach control frequency. adversely affect flight safety. 3-One pilot on tower frequency and the other on approach 2-When fuel endurance or weather will require an en route control frequency. or landing priority. 3-When distress conditions such asfire,mechanical 5777. When cleared to execute a published side-step failure, or structural damage occurs. maneuver, at what point is the pilot expected to commence this maneuver? 5784. It is the responsibility of the pilot and crew to report a near midair collision as a result of proximity of at least 1-At the published DH. 2-At the MDA published or a circling approach. 1-50 feet or less to another aircraft 3-As soon as possible after the runway environment is in 2-500 feet or less to another aircraft sight 3-1,000 feet or less to another aircraft 5778. If visual reference is lost while circling to land from 5785. When setting the altimeter, pilots should disregard an instrument approach, what action(s) should the pilot take? 1-effects of nonstandard atmospheric temperatures and pressures. 1-Make a climbing turn toward the landing runway until 2-corrections for static pressure systems. established on the missed approach course. 3-corrections for instrument error. 2-Turn toward the landing runway maintaining MDA, and if visual reference is not regained, perform missed ap- 5788. (Refer to figures 32, 35, and 36.) What is the CG in proach. percent of MAC for Load Condition WT-1? 3-Make a climbing turn toward the VOR/NDB, and request 1-26.0 percent MAC. further instructions. 2-27.1 percent MAC. 5779. What is the difference between a visual and a 3-27.9 percent MAC. contact approach? 5787. (Refer to figures 32, 35, and 36.) What is the CG in 1-A visual approach is an IFR authorization while a contact inches aft of datum for Load Condition WT-2? approach is a VFR authorization. 1-908.8 inches. 2-A visual approach is initiated by ATC while a contact 2-909.6 inches. approach is initiated by the pilot 3-910.7 inches. 3-Both are the same but classified according to the party initiating the approach. 5788. (Refer to figures 32, 35, and 38.) What is the CG in percent of MAC for Load Condition WT-3? 5780. Except during an emergency, when can a pilot expect landing Prinritr 1-27.8 percent MAC. 2-28.9 percent MAC. 1-When cleared for an IFR approach. 3-29.1 percent MAC. 2-When piloting a large heavy aircraft. 3-In turn, on a first come, first serve basis. 5789. (Refer to figures 32, 35, and 38.) What is the CG in inches aft of datum for Load Condition WT-4? 5781. Under what condition should a pilot on IFR advise ATC of minimum fuel status? 1-908.4 inches. 2-909.0 inches. 1-When the fuel supply becomes less than that required 3-909.5 inches. for IFR. 2-If the remaining fuel suggests a need for traffic or 5790. (Refer to figures 32, 35, and 36.) What is the CG in landing priority. percent of MAC for Load Condition WT-5? 3-If the remainingfuelprecludes any undue delay. 1-25.6 percent MAC. 5782. What isthe maximum acceptable tolerancefor 2-26.7 percent MAC. penetrating a domestic ADIZ? 3-27.2 percent MAC.

1-Plus or minus 10 miles; plus or minus 10 minutes. 5791. (Refer to figures 33, 35, and 36.) What is the gross 2-Plus or minus 20 miles;plus or minus 5 minutes. weight index for Load Condition WT-6? 3-Plus or minus 10 miles;plus or minus 5 minutes. 1-181,340.5 index. 2-156,545.0 index. 3-165,991.5 index.

55 65 5792. (Refer to figures 33, 35, and 36.) What is the CG in 5801. What is the maximum allowable weight that may be percent of MAC for Load Condition WT-7? carried on a pallet which has the dimensions of 76 X 78 1-21.6 percent MAC. inches? 2-22.9 percent MAC. Floor load limit - 188 lb/sq ft 3-24.0 percent MAC. Pallet weight - 93 lb Tledown dev6-es - 39 lb 5793. (Refer to figures 33, 35, and 36.) What is the CG in percent of MAC for Load Condition WT-8? 1-7,421.3 pounds. 2-7,250.3 pounds. 1-29.4 percent MAC. 3-7,328.7 pounds. 2-30.0 percent MAC. 3-31.3 percent MAC. 5802. What is the maximum allowable weight that may be carried on a pallet which has the dimensions of 83 X 95 5794. (Refer to figures 33, 35, and 36.) What is the gross inches? weight Index for Load Condition WT-9? Floor load limit - 184 lb/sq ft 1-189,755.2 Index. Pallet weight - 85 lb 2-158,797.9 index. Tiedown devices - 36 lb 3-188,565.5 index. 1-10,075.3 pounds. 5796. (Refer to figures 33, 35, and 36.) What is the CG in 2- 9,954.3 pounds. percent of MAC for Load Condition WT-10? 3- 10,028.6 pounds.

1-27.0 percent MAC. 5803. What is the maximum allowable weight that may be 2-27.8 percent MAC. carried on a pallet which has the dimensions of 81 X 84 3-28.0 percent MAC. inches? 5798. (Refer to figures 34, 35, and 36.) What is the CG in Floor load limit - 189 lb/sq ft percent of MAC for Load Condition WT-11? Pallet weight - 88 lb 1-28.8 percent MAC. Tiedown devices - 37 lb 2-27.5 percent MAC. 1-8,156.0 pounds. 3-28.8 percent MAC. 2-8,281.0 pounds. 3-8,093.0 pounds. 5797. (Refer to figures 34, 35, and 36.) What is the CG in percent of MAC for Load Condition WT-12? 5804. What is the maximum allowable weight that may be 1-25.8 percent MAC. carried on a pallet which has the dimensions of 76 X 74 2-28.3 percent MAC. inches? 3-27.5 percent MAC. Floor load limit - 178 lb/sq ft Pallet weight - 77 lb 5798. (Refer to figures 34, 35, and 36.) What is the CG in Tiedown devices - 29 lb percent of MAC for Load Condition WT-13? 1-6,787.8 pounds. 1-28.8 percent MAC. 2-6,873.7 pounds. 2-29.4 percent MAC. 3- 8,796.8 pounds. 3-30.1 percent MAC. 5805. What is the maximum allowable weight that may be 5799. (Refer to figures 34, 35, and 36.) What is the CG in carried on a pallet which has the dimensions of 81 X -1 percent of MAC for Load Condition WT-14? inches? 1-30.1 percent MAC. Floor load limit - 180 lb/sq ft 2-29.5 percent MAC. Pallet weight - 82 lb 3-31.5 percent MAC. Tiedown devices - 31 lb 6400. (Refer to figures 34, 35, and 36.) What is the CG in 1-8,403.7 pounds. Percent of MAC for Load Condition WT-15? 2-8,321.8 pounds. 1-32.8 percent MAC. 3-8,290.8 pounds. 2-31.5 percent MAC. 6806. (Refer to figure 37.) What is the new CG if the weight 3-29.5 percent MAC. is shifted from the forward to the aft compartment under Load Condition WS-1? 1-15.2 percent MAC. 2-28.9 percent MAC. 3-30.0 percent MAC.

56 66 51107. (Refer to figure 37.) What is the new CG if the weight 5815. (Refer to figure 37.) What is the new CG if the weight is shifted from the aft to the forward compartment under is removed from the forward compartment under Load Load Condition WS-2? Condition WS-5? 1-28.1 percent MAC. 1-31.9 percent MAC. 2-20.5 percent MAC. 2-19.1 percent MAC. 3-22.8 percent MAC. 3-35.2 percent MAC.

5808. (Refer to figure 37.) What is the new CG if the weight 5816. (Refer to figures 38, 40, 42, 43, 44, and 45.) What is is shifted from the forward to the aft compartment under the CG in inches from datum under Loading Condition Load Condition WS-3? BE-1? 1-29.2 percent MAC. 1Station 290.3. 2-33.0 percent MAC. 2Station 285.8. 3-28.6 percent MAC. 3Station 291.8.

5009. (Refer to figure 37.) What is the new CG if the weight 5817. (Refer to figures 38, 40, 42, 43, 44, and 45.) What is is shifted from the aft to the forward compartment under the CG in inches from datum under Loading Condition Load Condition WS-4? BE-2? 1-37.0 percent MAC. 1Station 295.2. 2-23.5 percent MAC. 2Station 292.9. 3-24.1 percent MAC. 3Station 293.0.

5810. (Refer to figure 37.) Where is the new CG if the 5818. (Refer to figures 38, 40, 42, 43, 44, and 45.) What is weight is shifted from the forward to the aft compartment the CG ininches from datum under Loading Condition under Load Condition WS-5? BE-3? 1 +19.15 index arm. 1Station 288.2. 2 +13.93 index arm. 2Station 285.8. 3 -7.92 index arm. 3Station 290.4.

5811. (Refer to figure 37.) What is the new CG if the weight 5819. (Refer to figures 38, 40, 42, 43, 44, and 45.) What is is removed from the forward compartment under Load the CG ininches from datum under Loading Condition Condition WS-1? BE-4? 1-27.1 percent MAC. 1Station 297.4. 2-26.8 percent MAC. 2Station 299.6. 3-30.0 percent MAC. 3Station 297.7.

5812. (Refer to figure 37.) Where is the new CG if the 5820. (Refer to figures 38, 40, 42, 43, 44, and 45.) What is weightis added to theaft compartment under Load the CG in inches from datum under Loading Condition Condition WS-2? BE-5? 1 +17.06 index arm. 1Station 288.9. 2 +14.82 index arm. 2Station 290.5. 3 +12.13 index arm. 3Station 289.1.

5813. (Refer to figure 37.) What is the new CG if the weight 5821(Refer to figures 38, 40, 42, 43, 44, and 45.) What is isaddedtotheforwardcompartmentunderLoad the CG shift if the passengers in row 1 are moved to seats Condition WS-3? in row 9 under Loading Condition BE-1? 1-11.4 percent MAC. 1-1.5 inches aft. 2-14.3 percent MAC. 2-5.6 inches aft. 3-14.5 percent MAC. 3-6.2 inches aft.

5814. (Refer to figure 37.) Where is the new CG if the 5822. (Refer to figures 38, 40, 42, 43, 44, and 45.) What is weight is removed from the aft compartment under Load the CG shift if the passengers in row 1 are moved to row 8, Condition WS-4? and the passengers in row 2 are moved to row 9 under Loading' Co. tuition BE-2? 1 +15.53 index arm. 2 +8.50 index arm. 1-9.2 inches aft. 3-- -3.51 index arm. 2-5.7 inches aft. 3-7.8 inches aft.

67 5823. (Refer to figures 38, 40, 42, 43, 44, and45.) What is 5832. (Refer to figures 39, 41, 43, 44, and 45.) What is the the CG shift if four passengers weighing 170pounds each CG shift if the cargo in section F is moved to sectionA. are added; two to seats in row 8 and two to seats inrow 7, and 200 pounds of the cargo in section G is added to the under Loading Condition BE-3? cargo In section B, under Loading Condition BE-7? 1-3.5 inches aft. 1-5.2 inches forward. 2-2.2 inches forward. 2-4.0 inches forward. 3-1.8 inches aft 3-8.0 inches forward.

5824. (Refer to figures 38, 40, 42, 43, 44, and 45.)What is 5833. (Refer to figures 39, 41, 43, 44, and 45.) What is the the CO shift if all passengers in rows 2 and 4 are deplaned CG if all cargo in sections A, B, J, K, and Lare off-loaded under Loading Condition BE-4? under Loading Condition BE-8? 1-2.6 inches aft 1Station 291.9. 2-2.5 inches forward. 2Station 292.7. 3-2.0 inches aft 3Station 294.5.

5825. (Refer to figures 38, 40, 42, 43, 44, and45.) What is 5834. (Refer to figures 39, 41, 43, 44, and 45.) What Is the the CG shift if the passengers in row 8 are moved to row 2, CG if cargo is loaded to bring sections F, 3, andH to and the passengers in row 7 are moved torow 1, under maximum capacity under Loading Condition BE-9? Loading Condition BE-5? 1Station 303.5. 1-1.0 inches forward. 2Station 301.6. 2-8.9 inches forward. 3Station 305.4. 3-6.5 inches forward. 5835. (Refer to figures 39, 41, 43, 44, and 45.) What is the 5826. (Refer to figures 39, 41, 43, 44, and 45.) What is the CG shift if the cargo in section G is moved tosection J CG in inches from datum under Loading ConditionBE-8? under Loading Condition BE-10? 1Station 296.5. 1-2.0 inches forward. 2Station 296.1. 2-2.3 inches aft. 3Station 297.0. 3-3.2 inches aft

5827. (Refer to figures 39, 41, 43, 44, and 45.)What is the 5838. (Refer to figures 41, 43, 45, and 46.) What limit is CG in inches from datum under LoadingCondition BE-7? exceeded under Loading Condition BE-11? 1Station 295.4. 1ZFW limit is exceeded. 2Station 300.2. 2Aft CG limit is exceeded at takeoff weight 3Station 298.0. 3Aft CG limit is exceeded at landing weight.

5828. (Refer to figures 39, 41, 43, 44, and 45.)What is the 5837. (Refer to figures 41, 43, 45, and 46.) What limits) CO in inches from datum under Loading Condition BE-8? is(are) exceeded under Loading Condition BE-12'i 1Station 298.9. 1ZFW limit is exceeded. 2Station 297.4. 2Landing aft CG limit is exceeded. 3Station 298.1. 3ZFW and miudmum takeoff weight limits are exceeded.

6829. (Refer to figures 39, 41, 43, 44, and 45.)What is the 5838. (Refer to figures 41, 43, 45, and 48.) What limit, if CG in inches from datum under Loading Condition BE-9? any, is exceeded under Loading Condition BE-13? 1Station 298.7. 1Takeoff forward CG limit is exceeded. 2Station 297.2. 2No limit is exceeded. 3Station 297.1. 3Landing aft CG limit is exceeded.

MO. (Refer to figures 39, 41, 43, 44, and 45.)What !a the 6339. (Refer to figass 41, 43, 45, and 46.) What limit(s) CG in inches from datum under Loading Condition BE-10? is(are) exceeded undo Loading Condition BE-14? 1Station 293.9. 1Maximum ZFW limit is exceeded. 2--Station 293.0. 2Takeoff forward CG Nmi is exceeded. 3Station 292.8. 3 Maximum landing weight and landing forward CGlimits are exceeded. 5631. (Refer to figures 39, 41, 43, 44, and 45.)What is the CO shift if 300 pounds ofcargo in section A is moved to section H under Loading Condition BE-6? 1-4.0 inches aft 2-2.5 inches aft. 3-4.3 inches aft.

68 56 5840. (Refer to figures 41, 43, 45, and 48.) What limit(s) 5849. (Refer to figures 47, 49, 50, and 51.) What is the CG is(are) exceeded under Loading Condition BE-15? shift if the passengers in row 1 are moved to row 4 under Loading Condition BL-4? 1--Moodmum takeoff weight limit is exceeded. 2--Modmum ZFW and takeoff forward CG limits are 1-1.1 inches aft. exceeded. 2-1.8 inches aft. 3 Maximum takeoff weight and takeoff forward CG limits 3-0.2 inch aft. are exceeded. 5850. (Refer to figures 47, 49, 50, and 51.) What is the CG 5841. (Refer to figures 47, 49, 5n and 51.) Where is the shiftif one passenger, weighing 100 pounds seated in longitudinal CG located under Jading Condition BL-1 I row Iis moved to row 3, under Loading Condition 61,5? 1Station 214.3. 1-1.0 inch aft. 2Station 235.8. 2-0.4 inch aft 3Station 237.8. 3-1.3 inches aft

5842. (Refer to figures 47, 49, 50, and 51.) Where is the 5851. (Refer to figures 48, 5t, 51, and 53.) What limits are longitudinal CG located under Loading Condition BL-2? exceeded under Loading Cond,lon BL-8? 1Station 237.8. 1Aft CG limits are exceeded at takeoff and landing. 2Station 238.5. 2Takeoff aft CG and landing forward CG limits are 3Staton 282.3. exceeded. 3 Maximum takeoff weight and takeoff aft CG limits are 5843. (Refer to figures 47, 49, 50, and 51.) Where is the exceeded. longitudinal CG located under Loading Condition BL-3? 5852. (Refer to figures 48, 50, 51, and 53.) What limit,if 1 Station 223.4. any, is exceeded under Loading Condition BL-7? 2Station 239.0. 3Station 240.3. 1No limits are exceeded. 2Forward CG limit is exceeded at landing only. 5844. (Refer to figures 47, 49, 50, and 51.) Where is the 3Forward CG limit is exceeded at takeoff and landing. longitudinal CG located under Loading Condition BL-4? 5853. (Refer to figures 48, 50, 51, and 53.) What limit,if 1Station 238.1. any, is ,xceeded under Loading Condition BL-8? 2Station 220.4. 3Station 238.5. 1No limits are exceeded. 2Forward CG limit is exceeded at landing only. 5845. (Refer to figures 47, 49, 50, and 51.) Where is the 3Forward CG limit is exceeded at takeoff and landing. longitudinal CG located under Loading Condition BL-5? 5854. (Refer to figures 48, 50, 51, and 53.) What limit,if 1Station 232.0. any, is exceeded under Loading Condition BL-9? 2--Station 235.4. 3Station 234.9. 1No limits are exceeded. 2Aft CG limit is exceeded at takeoff only. 5848. (Refer to figures 47, 49, 50, and 51.) What Is the CG 3Aft CG limitisexceededat takeoff and landing. shift if all passengers in row 1 are moved to row 4 under Loading Conditionr ..1? 5855. (Refer to figures 48, 50. 51, and 53.) What limit,if any, is exceeded under Load''. j Condition BL-10? 1-5.0 Indies aft. 2-4.1 inches aft. 1No limits are exceeded. 3-0.19 inch aft. 2Aft CG limit is exceeded at takeoff. 3Forward CG limit is exceeded at landing. 5847. (Refer to figures 47, 49, 50, and 51.) What is the CG shiftif one passenger weighing 150 pounds in row 2 is 5858. (Refer to figures 48, 49, 50, 51, and 52.) Given moved to row 4 under Loading Condition BL-2? Loading Condition BL-8, what it the effect on lateral CG if the outside passengers from wch row on the left side are 1-0.1 inch aft. deplaned? Deplaned passe' ver weights are 170 pounds 2-0.8 inch aft. arch. 3-1.1 inches aft. 100 shifts 1.5 inches right, out of limits. 5848. (Refer to figures 47, 49, FO, and 51.) What is the CG 2CG shifts 1.4 inches right, within limits. shift if all passengers in row 4 are moved to row 1 under 3CG shifts 1.F inches left, out of limits. Loading Condition BL-3? 1-3.7 inches forward. 2-0.4 inch forward. 3-3.9 inches forward.

59 q9 5857. (Refer to figures 48, 49, 50, 51, and 52.) Given 5865. (Refer to figures 54, 55, and 56.) What are Vi and Vs Loading Condition BL-7, what is the effect on lateral CG if speeds for Operating Condition A-5? additione. passengers, each weighing 200 pounds,are seated, one in each outside right seat ofsows 1,2, 3, 1V1 110.4 knots; Vs 110.9 knots. and 4? 2V1 109.6 knots; VR 112.7 knots. 3Vi 106.4 knots; Vs 106.4 knots. 1CG shifts 1.5 inches left, out of limits. 2CG shifts 0.2 inch right, within limits. 5866. (Refer to figure 55.) What is the STAB TRIM setting 3CG shifts 1.8 inches right, out of limits. for Operating Condition A-1?

511511. (Refer to figures 48, 49, 50, 51, and 52.) Given 1-29 percent MAC. Loading Condition BL-8, what is the effect on lateral CG ifa 2-32 percent MAC. passenger weighing 200 pounds is added to the outer left 3-36 percent MAC. seat of row 1, and a passenger weighing 220 pounds is added to the outer left seat of row 4? 5867. (Refer to figure 55.) What is the STAB TRIM setting for Operating Condition A-2? 1CG shifts 1.5 inches left, out of limits. 2CG shifts 1.2 inches left, within limits. 1-26 percent MAC. 3CG shifts 1.0 inch left, within limits. 2 -20 percent MAC. 3-22 percent MAC. 5859. (Refer to figures 48, 49, 50, 51, and 52.) Given Loading Condition BL-9, what is the effect on lateral CG if 5868. (Refer to figure 55.) What is the STAB TRIM setting passengers, each weighing 160 pounds, are added to the for Operating Condition A-3? outer left seats of rows 1 and 2; and Passengers, each 1-18 percent MAC. weighing 180 pounds are added to the cute "ight seats of 2-20 percent MAC. rows 3 and 4? 3-22 percent MAC. 1CG shifts 0.14 inch left. 2CG shifts 0.15 inch right 5869. (Refer to figure 55.) What is the STAB TRIM setting 3CG does not shift. for Operating Condition A-4? 1-26 percent MAC. 5850. (Refer to figures 48, 49, 50, 51, and 52.) Given 2-22 percent MAC. Loading Condition BL-10, what is the effect on lateral CG if 3-18 percent MAC. a passenger, weighing 240 pounds, is shifted from the outer right seat of row 4 to the outer left seat ofrow 1? 5870. (Refer to figure 55.) What is the STAB TRIM setting for Operating Condition A-5? 1CG shifts 1.1 inches left, within limits. 2CG shifts 1.5 inches left, out of limits. 1-26 percent MAC. 3CG shifts 1.7 inches left, out of limits. 2-30 percent MAC. 3-32 percent MAC. 5861. (Refer to figures 54, 55, and 56.) Whatare V1 and VR speeds for Operating Conditions A-1? 5871. (Refer to figures 54, 57, and 58.) What is the max takeoff EPR for Operating Condition G-1? 1V1 123.1 knots; Vs 125.2 knots. 2V1 120.5 knots; Vs 123.5 knots. 1Engines 1 and 3, 2.22; engine 2, 2.16. 3V1 122.3 knots; Vs 124.1 knots. 2Engines 1 and 3, 2.22; engine 2, 2.21. 3Engines 1 and 3, 2.15; engine 2, 2.09. 5862. (Refer to figures 54, 55, and 56.) Whatare V1 and VR speeds for Operating Condition A-2? 5872. (Refer to figures 54, 57, and 58.) What is the max takeoff EPR for Operating Condition G-2? 1V1 129.7 knots; Vs 134.0 knots. 2V1 127.2 knots; Vs 1332 knots. 1Engines 1 and 3, 2.15; engine 2, 2.16. 3V, 127.4 knots; Vs 133.6 knots. 2Engines 1 and 3, 2.18; engine 2, 2.13. 3Engines 1 and 3, 2.14; engine 2, 2.11. 5863. (Refer to figures 54, 55, and 56.) Whatare V1 and VR speeds for Operating Condition A-3? 5873. (Refer to figures 54, 57, and 58.) What is the max takeoff EPR for Operating Condition G-3? 1V, 136.8 knots; Vs 141.8 knots. 2V1 134.8 knots; Vs 139.0 knots. 1Engines 1 and 3, 2.08; engine 2, 2.05. 3V1 133.5 knots; VR 141.0 knots. 2Engines 1 and 3, 2.14; engine 2, 2.10. 3Engines 1 and 3, 2.18; engine 2, 2.07. 5864. (Refer to figures 54. 65, and 56.) What are V1 andVR speeds for Operating Condition A-4? 5874. (Refer to figures 54, 57, and 58.) What is the max takeoff EPR for Operating Condition G-4? 1V1 128.0 knots; Vs 130.5 knots. 2V, 129.9 knots; VR 133.4 knots. 1Engines 1 and 3, 2.23; engine 2, 2.21. 3V1 128.8 knots; Vs 131.1 knots. 2Engines 1 and 3, 2.26; engine 2, 2.25. 3Engines 1 and 3, 2.24; engine 2, 2.24.

60 70 5875. (Refer to figures 54, 57, and 58.) What is the max 5885. (Refer to figures 57 and 58.) What is the STAB TRIM takeoff EPR for Operating Condition G-5? setting for Operating Condition G-5? 1Engines 1 and 3, 2.27; engine 2, 2.18. 1-3-1/4 ANU. 2Engines 1 and 3, 2.16; engine 2, 2.14. 2-2-3/4 ANU. 3Engines 1 and 3, 2.23; engine 2, 2.22. 3-2-1/2 ANU.

5878. (Refer to figures 54, 57, and 58.) What is the takeoff 5886. (Refer to figures 54, 59, and 61.) What is the takeoff safety speed for Operating Condition G-1? EPR for Operating Condition R-1? 1-122 knots. 1-2.04. 2-137 knots. 2-2.00. 3-133 knots. 3-2.01.

5877. (Refer to figures 54, 57, and 58.) What is the rotation 5887. (Refer to figures 54, 59, and 61.) What is the takeoff speed for Operating Condition G-2? EPR for Operating Condition R-2? 1-150 knots. 1-2.16. 2-154 knots. 2-2.19. 3-155 knots. 3-2.18.

5878. (Refer to figures 54, 57, and 58.) What are VI, VII, 5888. (Refer to figur is 54, 59, and 61.) What is the takeoff and V, speeds for Operating Condition G-3? EPR for Operating Co.sdition R-3? 1-134, 134, and 145 knots. 1-2.01. 2-134, 139, and 145 knots. 2-2.06. 3-132, 132, and 145 knots. 3-2.04.

6879. (Refer to figures 54, 57, and 58.) What are V1 and V2 5889. (Refer to figures 54, 59, and 61.) What is the takeoff speeds for Operating Condition G-4? EPR for Operating Condition R-4? 1-133 and 145 knots. 1-2.08. 2-127 and 141 knots. 2-2.06. 3-132 and 146 knots. 3-2.11.

5880. (Refer to figures 54, 57, and 58.) What are rotation 5890. (Refer to figures 54, 59, and 61.) What is the takeoff and V, bug speeds for Operating Condition G-5? EPR for Operating Condition R-5? 1-120 and 134 knots. 1-1.98. 2-119 and 135 knots. 2-1.95. 3-135 and 135 knots. 3-1.96.

5881. (Refer to figures 57 and 58.) What is the STAB TRIM 5891. (Refer to figures 54, 59, and 61.) What is the takeoff setting for Operating Condition G-1? safety speed for Operating Condition R-1? 1-4 ANU. 1-128 knots. 2-4-1/2 ANU. 2-121 knots. 3-4-3/4 ANU. 3-133 knots.

5882. (Refer to figures 57 and 58.) What is the STAB TRIM 5892. (Refer to figures 54, 59, and 61.) What is the rotation setting for Operating Condition G-2? speed for Coeratirig Condition R-2? 1-6-1/2 ANU. 1-147 knots. 2 -7.1/4 ANU. 2-152 knots. 3-5-3/4 ANU. 3-146 knots.

5883. (Refer to figures 57 and 58.) What is the STAB TRIM 5893. (Refer to figures 54, 59. and 61.) What are V,, VR, setting for Operating Condition G-3? and V2 speeds for Operating Condition R-3? 1-3-3/4 ANU. 1-143, 143, and 147 knots. 2-4 ANU. 2-138, 138, and 142 knots. 3-4-1/4 ANU. 3-136, 138, and 143 knots.

5884. (Refer to figures 57 and 58.) What is the STAB TRIM setting for Operating Condition G-4? 1-2-3/4 ANU. 2-4 ANU. 3-2-1/2 ANU.

61 5894. (Refer to figures 54, 59, and 61.) What are critical 5903. (Refer to figures 60, 62, and 63.) What is the ground engine failure and takeoff safety speeds for Operating distance covered during en routeclimbfor Operating Condition R-4? Condition V-3? 1-131 and 133 knots. 1-95 miles. 2-123 and 134 knots. 2-79 miles. 3-122 and 130 knots. 3-57 miles.

5895. (Refer to figures 54, 59, and 61.) What are rotation 5904. (Refer to figures 60, 62, and 63.) What is the ground and V, bug speeds for Operating Condition R-5? distance covered during en route climbfor Operating Condition -.4? 1-138 and 143 knots. 2-138 and 138 knots. 1-63 miles. 3-134 and 141 knots. 2-53 miles. 3-65 miles. 5898. (Refer to figures 59 and 61.) What is the STAB TRIM setting for Operating Condition R-1? 5905. (Refer to figures 60, 62, and 63.) What is the ground 1-8 ANU. distance covered during en routeclimbfor Operating 2-7-5/8 ANL' Condition V-5? 3-7-3/4 ANU. 1-70 miles. 2-47 miles. 5897. (Refer to figures 59 and 61.) What is the STAB TRIM 3-61 miles. setting for Operating Condition R-2? 1-5-3/4 ANU. 5908. (Refer to figures 60, 62, and 63.) How much fuel is 2-7 ANU. burned during en route climb for Operating Condition V-1? 3-8-3/4 ANU. 1-4,100 pounds. 2-3,600 pounds. 5898. (Refer to figures 59 and 61.) What is the STAB TRIM 3-4,000 pounds. setting for Operating Condition R-3? 1-3 ANU. 5907. (Refer to figures 60, 62, and 63.) How much fuel is 2-4-1/2 ANU. burned during en route climb for Opdrati,12 cti.ndition V-2? 3-5 ANU. 1-2,250 pounds. 2-2,600 pounds. 5899. (Refer to figures 59 and 61.) What is the STAB TRIM 3-2,400 pounds. setting for Operating Condition R-4? 1-4-1/4 ANU. 5908. (Refer to figures 60, 62, and 63.) What is the aircraft 2-4-1/2 ANU. weight at the top of climb for Operating Condition V-3? 3-5 ANU. 1-82,100 pounds. 2-82,500 pounds. 5900. (Refer to figures 59 and 61.) Whet is the STAB TRIM 3-82,200 pounds. setting for Operating Condition R-5? 1-6-3/4 ANU. 5909. (Refer to figures 60, 62, and 63.) What is the aircraft 2-8 M U. weight at the top of climb for Operating Condition V-4? 3-7-1/a ANU. 1-102,900 pounds. 2-102,600 pounds. 5901. (Refer to figures 60, 62, and 63.) What is the ground 3-103,100 pounds. distance covered during en routeclimbfor Operating Condition V-1? 5910. (Refer to figures 60, 62, and 63.) What is the aircraft 1-145 miles. weight at the top of climb for Operating Condition V-5? 2-137 miles. 1-73,000 pounds. 3-134 miles. 2-72,900 pounds. 3-72,800 pounds. 5902. (Refer to figures 60, 62, and 63.) What is the ground distance coveredduring en route climbfor Operating 5911. (Refer to figures 64 and 66.) What is the max climb Condition V-2? EPR for Operating Conditions T-1? 1-84 miles. 1-1.96. 2-85 miles. 2-2.04. 3-89 miles. 3 -1.90.

7262 5012. (Refer to figures 84 and 66.) What is the max 5921. (Refer to figures 65, 67, and 68.) What is the aircraft continuous EPR for Operating Condition T-2? weight at the top of climb for Operating Condition W-1? 1-2.10. 1-81,600 pounds. 2-1.99. 2-81,400 pounds. 3-2.02. 3-81,550 pounds.

5913. (Refer to figures 64 and 66.) While is the max cruise 5922. (Refer to figures 65, 67, and 68.) What is the aircraft EPR for Operating Condition T-3? weight at the top of climb for Operating Condition W-2? 1-2.11. 1-82,775 pounds. 2-2.02. 2-83,650 pounds. 3-1.90. 3-83,800 pounds.

5914. (Refer to figures 64 and 66.) What Is the max climb 5923. (Refer to figures 65, 67, and 68.) What is the aircraft EPR for Operating Condition T-4? weight at the top of climb for Operating Condition W-3? 1-2.20. 1-75,750 pounds. 2-2.07. 2-75,900 pounds. 3-2.06. 3-76,100 pounds. 5915. (Refer to figures 64 and 66.) What is the max 5924. (Refer to figures 65, 67, and 68.) What is the aircraft continuous EPR for Operating Condition T-5? weight at the top of climb for &orating Condition W-4? 1-2.00. 1-86,150 pounds. 2-2.04. 2-86,260 pounds. 3-1.98. 3-86,450 pounds.

5916. (Refer to figures 65, 67, and 68.) What is the ground 5925. (Refer to figures 65, 67, an 1 S8.) What is the aircraft distance covered during en routeclimb for Operating weight at the top of climb for Operating Condition W-5? Condition W-1? 1-89,900 pounds. 1-104.0 miles. 2-90,000 pounds. 2-99.2 miles. 3-90,100 pounds. 3-109.7 miles. 5926. (Refer to figures 69 and 71.) What is the trip time for 5917. (Refer to figures 85, 67, and 68.) What is the ground Operating Condition X-1? distance covered during en routeclimb forOperating 1-4 hours 5 minutes. Condition W-2? 2-4 hours 15 minutes. 1-85.8 miles. 3-4 hours. 2-87.8 miles. 3-79.4 miles. 5927. (Refer to figures 69and 71.) What is the trip time for Operating Condition X-2? 5919. (Refer to figures 65, 67, and 68.) What is the ground 1-5 hours 5 minutes. distance covered during en routeclimb for Operating 2-6 hours 15 minutes. Condition W-3? 3-5 hours 55 minutes. 1-88.4 miles. 2-84.2 miles. 5923. (Refer to figures 69and 71.) What Is the trip time for 3-85.1 miles. Operating Condition X-3? 1-4 hours 15 minutes. 5919. (Refer to Wee 85, 67, and 68.) What is the ground 2-3 hours 40 minutes. distance covered during en routeclimb for Operating 3-4 hours. Condition W-4? 1-58.4 miles. 5929. (Refer to figures 89and 71.) What is the trip time for 2-61.4 miles. Operating Condition X-4? 3-80.3 mast 1-6 hours 50 minutes. 2-5 hours 45 minutes. 5620. (Refer to figures 65, 67, and 88.) What is the ground 3-5 hours 30 minutes distance covered during en routeclimb for Operating Condition W-5? 5930. (Refer to figures 69 and 71.) What is the trip time for 1-68.0 mass. Operating Condition X-5? 2-73.9 miles. 1-2 hours 55 minutes. 3-06.4 miles. 2-3 hours 10 minutes. 3-2 hours 50 minutes.

4 r 63 ...... ; 73 5931. (Refer to figures 69 and 71.) What is the trip fuel for 5941. (Refer to figures 72 and 74.) What is the Operating Condition X-1? trip time corrected for wind under Operating Condition Z-1? 1-25,000 pounds. 1-58.1 minutes. 2-26,000 pounds. 2-51.9 minutes. 3-24,000 pounds. 3-54.7 minutes. 5932. (Refer to figures 69 and 71.) What is the trip fuel for 5942. (Refer to figures 72 and 74.) What Operating Condition X-2? is the trip time corrected for wind under Operating Condition Z-2? 1-33,000 pounds. 1-1 hour 35 minutes. 2-28,000 pounds. 2-1 hour 52 minutes. 3-35,000 pounds. 3-1 hour 46 minutes. 5933. (Refer to figures 69 and 71.) What is the trip fuel for 5943. (Refer to figures 72 and 74.) What is Operating Condition X-3? the trip time corrected for wind under Operating Condition Z-3? 1-36,000 pounds. 1-2 hours 9 minutes. 2-34,500 pounds. 2-1 hour 59 minutes. 3-33,000 pounds. 3-1 hour 52 minutes. 5934. (Refer to figures 69 and 71.) What is the trip fuel for 5944. (Refer to figures 72 and 74.) What Operating Condition X-4? is the trip time corrected for wind under Operating Condition Z-4? 1-33,000 pounds. 1-48.3 minutes. 2-31,500 pounds. 2-50.7 minutes. 3-34,000 pounds. 3-51.3 minutes. 5935. (Refer to figures 69 ind 71.) What is the trip fuel for 5945. (Refer to figures 72 and 74.) What is Operating Condition X-5? the trip time corrected for wind under Operating Condition Z-5? 1-15,000 pounds. 1-1 hour 11 minutes. 2-20,000 pounds. 2-58 minutes. 3-19,000 pounds. 3-82 minutes. 5936. (Refer to figures 70 and 73.) What is the turbulent air 5946. (Refer to figures 72 and 74.) What is the penetration NI power setting for estimated Operating Condition 0-1? fuel consumption for Operating Condition 2-1? 1-82.4 percent 1-5,230 pounds. 2-84.0 percent 2-5,970 pounds. 3-84.8 percent 3-5,550 pounds. 5937. (Refer to figures 70 and 73.) What is the turbulent air 5947. (Refer to figures 72 and 74.) What is the estimated penetration NI power setting for Operating Condition 0-2? fuel consumption for -Operating Condition Z-2? 1-78.2 percent. 1-10,270 pounds. 2-75.2 percent 2 -9,660 pounds. 3-78.7 percent. 3-10,185 pounds. 5936. (Refer to figures 70 and 73.) What is the turbulent air 5948. (Refer to figures 72 and 74.) What is the penetration NI power setting for Operating estimated Condition 0-3? fuel consumption for Operating Condition Z-3? 1-77.8 percent 1-12,300 pounds. 2-82.6 percent 2-11,300 pounds. 3-84.2 percent 3-13,990 pounds. 5939. (Refer to figures 70 and 73.) What is the turbulent air 5949. (Refer to figures 72 and 74.) What is the penetration N1 power setting for Operating estimated Condition 0-4? fuel consumption for Operating ConditionZ-4? 1-76.8 percent 1-4,950 pounds. 2-75.4 percent. 2-5,380 pounds. 3-74.0 percent. 3-5,230 pounds. 5940. (Refer to figures 70 and 73.) What is the Turbulent air 5950. (Refer to figsms 72 and 74.) What is the penetration NI power setting for Operating estimated Condition 0-5? fuel consumption for Operating Condition Z-5? 1-70.9 percent 1-6,250 pounds. 2-72.9 percent 2-5,380 pounds. 3-71.6 percent. 3-7,120 pounds. ea 74 5951. (Refer to figures 75 and 78.) What is the total time 5960. (Refer to figures 75 and 78.) What is the approximate from startingto thealternate through completing the landing weight for Operating Condition L-5? approach for Operating Condition L-1? 1-78,800 pounds. 1-30 minutes. 2-77,000 pounds. 2-45 minutes. 3-76,800 pounds. 3-29 minutes. 5961. (Refer tofigures 76 and79.) What arethe 5952. (Refer to figures 75 and 78.) What is the total time recommended IAS and EPR settings for holding under from startingtothealternatethrough completing the Operating Condition H-1? approach for Operating Condition L-2? 1-284 knots and 1.80 EPR. 1-38 minutes. 2-259 knots and 1.73 EPR. 2-51 minutes. 3-261 knots and 1.81 EPR. 3-40 minutes. 5962. (Refertofigures 76 and79.)What arethe 5953. (Refer to figures 75 and 78.) What is the total time recommended IAS and EPR settings for holding under from starting to the alternate through completing the Operating Condition H-2? approach for Operating Condition L-3? 1-257 knots and 1.60 EPR. 1-1 how. 2-258 knots and 1.86 EPR. 2-1 hour 9 minutes. 3-253 knots and 1.57 EPR. 3-1 hour 24 minutes. 5963. (Refertofigures 76 and79.)What are the 5954. (Refer to figures 75 and 78.) What is the total time recommended IAS and EPR settings for holding under from starting to thealternatethrough completing the Operating Condition H-3? approach for Operating Condition L-4? 1-228 knots and 1.30 EPR. 1-34 minutes. 2-230 knots and 1.31 EPR. 2-19 minutes. 3-234 knots and 1.32 EPR. 3-20 minutes. 5964. (Refertofigures76 and79.)What arethe 5955. (Refer to figures 75 and 78.) What is the total time recommended IAS and EPR settings for holding under from starting to the alternatethrough completing the Operating Condition H-4? approach for Operating Condition L-5? 1-219 knots and 1.44 EPR. 1-1 hour 10 minutes. 2-216 knots and 1.42 EPR. 2-48 minutes. 3-220 knots and 1.63 EPR. 3-55 minutes. 5965. (Refertofigures76 and79.)What arethe 5956. (Refer to figures 75 and 78.) What is the approximate recommended IAS and EPR settings for holding under landing weight for Operating Condition L-1? Operating Condition H-5? 1-79,000 pounds. 1-245 knots and 1.85 EPR. 2-83,500 pounds. 2-237 knots and 1.61 EPR. 3-81,500 pounds. 3-24f., knots and 1.67 EPR.

5957. (Refer to figures 75 and 78.) What is the approximate 5966. (Refer to figures 76 and 79.) What is the approximate landing weight for Operating Condition L-2? fuel consumed when holding under Operating Condition H-1? 1-65,200 pounds. 2-88,100 pounds. 1-3,500 pounds. 3-89,600 pounds. 2-4,880 pounds. 3-2,630 pounds. 5951 (Refer to figures 75 and 78.) What is the approximate landing weight for Operating Condition L-3? 5967. (Refer to figures 76 and 79.) What is the approximate fuel consumed when holding under Operating Condition 1-80,300 pounds. H-2? 2-85,400 pounds. 3-77,700 pounds. 1-5,100 pounds. 2-3,400 pounds. 5969. (Refer to figures 75 and 78.) What is the approximate 3-5,250 pounds. landing weight for Operating Condition 1-4? 1-73,300 pounds. 1-74,190 pounds. 3-73,500 pounds.

85 75 5968. (Refer to figures 78 and 79.) What is the approximate 5976. (Refer to figures 77 and 80.) What is the approximate fuel consumed when holding under Operating Condition fuel consumed when holding under Operating Condition H-3? 0-1? 1-3,090 pounds. 1-1,625 pounds. 2-8,950 pounds. 2-1,950 pounds. 3-6,880 pounds. 3-2,440 pounds. 5969. (Refer to figures 78 and 79.) What is the approximate 5977. (Refer to figures 77 and 80.) What is the fuel consumed when holding approximate under Operating Condition fuel consumed when holding under Operating Condition H-4? 0-2? 1-3,190 pounds. 1-2,250 pounds. 2-3,050 pounds. 2-2,500 pounds. 3-2,550 pounds. 3-3,000 pounds.

5970. (Refer to figures 76 and 79.) Whatis the approximate 5978. (Refer to figures 77 and 80.) What is the fuel consumed when holding under approximate Operating Condition fuel consumed when holding under OperatingCondition H-5? 0-3? 1-3,170 pounds. 1-2,940 pounds. 2-7,380 pounds. 2-2,520 pounds. 3-5,540 pounds. 3-3,250 pounds. 5971. (Refertofigures 77 and80.) What arethe 5979. (Refer to figures 77 and 80.) What is the approximate recommended IAS and EPR settings for holding cider fuel consumed when holding underOperating Condition Operating Condition 0-1? 0-4? 1-221 knots and 1.83 EPR. 1-2,870 pounds. 2-223 knots and 2.01 EPR. 2-2,230 pounds. 3-217 knots and 1.81 EPR. 3-1,440 pounds. 5972. (Referto figures77 and80.) What arethe 5980. (Refer to figures 77 and 80.) What is the approximate recommended IAS and EPR settings forholding under fuel consumed when holding under Operating Condition Operating Condition 0-2? 0-5? 1-210 knots and 1.57 EPR. 1-2,950 pounds. 2-210 knots and 1.51 EPR. 2-2,870 pounds. 3-210 knots and 1.45 EPR. 3-2,400 pounds. 5973. (Referto figures77 and80.)What arethe 5981. (Refer to figure 81.) How many minutes of dump time recommended IAS and EPR settingsfor holding under is required to reach a weight of 144,500 pounds? Operating Condition 0-3? Initial Weight. 180,500 lb 1-217 knots and 1.50 EPR. Zero Fuel Weight 2-215 knots and 1.44 EPR. 125,500 lb 3-218 knots and 1.40 EPR. 1-13 minutes. 2-15 minutes. 5974. (Refertofigures77 and80.) What arethe 3-18 minutes. recommended IAS and EPR settingsfor holding under Operating Condition 0-4? 5982. (Refer to figure 81.) How many minutes of dump time is required to reduce fuel load to 25,000 pounds? 1-223 knots and 1.33 EPR. 2-225 knots and 1.33 EPR. Initial Weight. 179,500 lb 3-220 knots and 1.28 EPR. Zero Fuel Weight 136,500 ib 1-10 minutes. 5975. (Refer tofigures77 and 80.) What arethe recommended IAS and EPR settingsfor holding under 2-9 minutes. Operating Condition 0-5? 3-8 minutes.

1-219 knots and 1.28 EPR. 5983. (Refer to figure 81.) How many minutes of dump time 2-214 knots and 1.28 EPR. is required to reach a weight of 151,500 pounds? 3-218 knots and 1.27 EPR. Initial Weight. 181,500 lb Zero Fuel Weight 126,000 lb 1-15 minutes. 2-14 minutes. 3-13 minutes. ;76 138 5984. (Refer to figure 81.) How many minutes of dump time 5992. (Refer to figures 83 and 85.) What are descent fuel is required to reduce fuel load to 16,000 pounds? and distance under Operating Condition S-2?

Initial Weight 175,500 lb 1.-1,440 pounds, 104 NAM. Zero Fuel Weight. 138,000 lb 2-1,500 pounds, 118 NAM. 3-1,400 pounds, 98 NAM. 1-9 minutes. 2-10 minutes. 5993. (Refer to figures 83 and 85.) What are descent fuel 3-8 minutes. and distance under Operating Condition S-3?

5985. (Refer to figure 81.) How many minutes of dump time 4-1,490 pounds, 118 NAM. is required to reach a weight of 144,000 pounds? -1,440 pounds, 110 NAM. 3-1,550 pounds, 127 NAM. Initial Weight. 178,000 lb Zero Fuel Weight 121,000 lb 5994. (Refer to figures 83 and 85.) What are descent time and distance under Operating Condition S-4? 1-15 minutes. 2-14 minutes. 1-22 minutes, 110 NAM. 3-13 minutes. 2-21 minutes, 113 NAM. 3-24 minutes, 129 NAM. 591116. (Refer to figures 82 and 84.) What is the approximate level-off pressure altitude after drift-down under Operating 5995. (Refer to figures 83 and 85.) What are descent fuel Condition 0-1? and distance under Operating Condition S-5? 1-19,400 feet. 1-1,420 pounds, 97 NAM. 2-18,000 feet. 2-1,440 pounds, 102 NAM. 3-20,200 feet 3-1,390 pounds, 92 NAM.

59e'. (Refer to figures 82 and 84.) What is the approximate 5996. (Refer to figures 86 and 87.) What is the go-around level-off pressure altitude after drift-down under Operating EPR for Operating Condition L-1? Condition D-2? 1-1.98 EPR. 1-14,700 feet 2-2.01 EPR. 2-17,500 feet 3-2.00 EPR. 3-18,300 feet 5997. (Refer to figures 86 and 87.) What is the go-around 5968. (Refer to figures 82 and 84.) What is the approximate EPR for Operating Condition L-2? level-off pressure altitude after drift -down under Operating Condition D-3? 1-2.15 EPR. 2-2.03 EPR. 1-22,200 feet 3-2.06 EPR. 2-19,800 feet 3-21,600 feet 5998. (Refer to figures 86 and 87.) What is the go-around EPR for Operating Condition L-3? 5989. (Refer to figures 82 and 84.) What is the approximate level-off pressure altitude after drift -down under Operating 1-2.03 EPR. Condition D-4? 2-2.07 EPR. 3-2.05 EPR. 1-27,900 feet. 2-22,200 feet. 5999. (Refer to figures 86 and 87.) What is the go-around 3-24,400 feet EPR for Operating Condition L-4?

5990. (Refer to figures 82 and 84.) What is the approximate 1-2.05 EPR. level-off pressure altitude after drift-down under Operating 2-2.12 EPR. Condition D-5? 3-2.09 EPR. 1-8,800 feet 6000. (Refer to figures 86 and 87.) What is the go-around 2-9,800 feet EPR for Operating Condition '--5? 3-13,000 feet. 1-2.00 EPR. 5991. (Refer to figures 83 and 85.) What are descent time 2-2.07 EPR. and distance under Operating Condition S-1? 3-2.04 EPR. 1-24 minutes, 118 NAM. 6001. (Refer to figures 86, 87, and 118.) What is Van for 2-28 minutes, 125 NAM. Operating Condition L-1? 3-25 minutes, 118 NAM. 1-143 knots. 2-144 knots. 3-145 knots.

87 744'17 6002. (Refer to figures 86, 87, and 118.) What is reference 6010. (Refer to figure 88.) How many feet will remain after speed For Operating Condition L-2? landing on a 7,200-foot dry runway with spoilers inoperative 1-140 knots. at 118,000 pounds gross weight? 2-145 knots. 1-4,200 feet. 3-148 knots. 2-4,500 feet 3-4,750 feet 6003. (Wier to figures 86, 87, and 118.) What is VRE,+20 for Operating Condition L-3? 6011. (Refer to figure 90.) What is the transition distance 1-151 knots. when landing on an icy runway at a gross weight of 2-169 knots. 134,000 pounds? 3-149 knots. 1-400 feet 2-950 feet 6004. (Refer to figures 86, 87, and 118.) What isVng + 10 3-1,350 feet. for Operating Condition L-4? 1-152 knots. 6012. (Refer to figure 89.) How many feet will remain after 2-138 knots. landing on a 6,000-foot wet runway with reversers inoper- 3-148 knots. ative at 122,000 pounds gross weight? 1-2,200 feet. 6006. (Refer tofigures86,87, and118.) Whatis 2-2,750 feet. maneuvering speed for Operating Condition L-5? 3-3,150 feet. 1-124 knots. 2-137 knots. 6013. (Refer to figure 90.) What is the maximum landing 3-130 knots. weight which will permit stopping 500 feet short of the end of a 5,200-foot icy runway? 6006. (Refer to figure 89.) Which of the following configura- 1-124,000 pounds. tions will result in the shortest landing distanceover a 2-137,000 pounds. 50-foot obstacle to a wet runway? 3-108,000 pounds. 1- Brakes and spoilers at 122,500 poundsgross weight. 6014. (Refer to figure 88.) What is the maximum landing 2-Brakes and reversers at 124,000 poundsgross weight weight which will permit stopping 2,000 feet short of the end 3-Brakes, spoilers and reversers at 131,000 poundsgross weight of a 5,400-foot dry runway with reversers and spoilers inoperative? 6007. (Refer to figures 88 and 89.) Which conditions will 1-117,500 pounds. result in the shortest landing distance at a ,veight of 2-136,500 pounds. 132,500 pounds? 3-139,500 pounds. 1-Dry runway using brakes andreversers. 2-Dry runway using brakes and spoilers. 6015. (Refer to figure 90.) What is the landing distance on an icy runway with reversers inoperative at a landing weight 3-Wet runway usingbrakes,spoilers andreversers. of 125,000 pounds? 6006. (Refer to figure 90.) Which configuration will result in 1-4,500 feet. a landing distance of 5,900 feet over a 50-foot obstacle to 2-4,750 feet. an icy runway? 3-5,800 feet. 1-Use of three reversers at 131,000 poundsgross weight 6016. (Refer to figure 91.) How much will landing distance 2-Use of brakes and spoilers at 125,000 poundsgross weight be reduced by using 15° of flaps rather than 0° flaps ata landing weight of 119,000 pounds? 3-Use of three reversers at 133,000 poundsgross weight 1-500 feet. 6000. (Refer to figure 88.) How muchlonger is the dry 2-800 feet. runway landing distance using brakes only comparedto 3-2,700 feet. using brakes awl reversers at 114,000 poundsgross weight? 6017. (Refer to figure 91.) What is the ground roll when 1-1,150 feet landingwith15'offlapsatalandingweightof 2-500 feet. 122,000 pounds? 3-300 feet. 1-1,750 feet. 2-2,200 feet 3-2,750 feet.

7868 8018. (Refer to figures 91 and 93.) What approach speed 8028. (Refer to figure 93.) What thrustisrequired to and ground roll will be needed when landing at a weight of maintainlevelflightat 140,000 pounds, with gear up, 140,000 pounds if flaps are not used? flaps 25', and an airspeed of 172 knots? 1-138 knots and 3,900 feet 1-13,700 pounds. 2-153 knots and 2,900 feet 2-18,600 pounds. 3-183 knots and 2,900 feet 3-22,000 pounds.

6019. (Refer to figure 91.) How much more runway will be 6027. (Refer to figure2.) What thrustisrequired to used to land with 0' flaps rather than 15° of flaps at a maintainlevelflightat 1:0,000 pounds, with gear up, landing weight of 126,000 pounds? flaps 25', and an airspeed of 152 knots? 1-900 feet 1-14,500 pounds. 2-1,800 feet. 2-15,900 pounds. 3-2,700 feet. 3-16,700 pounds.

8020. (Refer to figures 91 and 93.) What approach speed 6028. (Refer to figure93.) What thrustisrequired to and landing distance will be needed when landing at a maintain level flight at 140,000 pounds, with gear down, weight of 140,000 pounds with 15° of flaps? flaps 25', and an airspeed of 162 knots? 1-123 knots and 3,050 feet. 1-17,400 pounds. 2-138 knots and 3,050 feet 2-19,500 pounds. 3-153 knots and 2,050 feet 3-22,200 pounds.

6021. (Refer to figure 92.) What is the maximum indicated 6029. (Refer to figure93.) What thrustisrequired to airspeed available when maintaining a 3' glide slope at a maintain level flight at 140,000 pounds, with gear down, weight of 110,000 pounds? flaps 25°, and an airspeed of 145 knots? 1-136 knots. 1-16,500 pounds. 2-132 knots. 2-18,100 pounds. 3-139 knots. 3-18,500 pounds.

6022. (Refer to figure 93.) What is the maximum indicated 6030. (Refer to figure 93.) What is the change of total drag airspeed available when maintaining a 3' glide slope at a for a 140,000 pound airplane when configuration is changed weight of 140,000 pounds? from flaps 30', gear down, to flaps 0°, gear up, at a constant airspeed of 160 knots? 1-127 knots. 2-149 knots. 1-13,500 pounds. 3-156 knots. 2-13,300 pounds. 3-15,300 pounds. 6023. (Refer to figure 93.) What is the thrust required to maintain a 3' glide slope at 140,000 pounds, with gear 6031. (Refer to figure 94.) Given the following conditions, down, flaps 30', and an airspeed of VI," +30 knots? what is the minimum torque for takeoff? 1-13,300 pounds. Pressure altitude 9,000 ft 2-16,200 pounds. Temperature (OAT) +3' C 3-17,700 pounds. Ice vanes Extended

6024. (Refer to figure 92.) What is the thrust required to 1-3,100 ft-lb. maintain a 3° glide slope at 110,000 pounds, with gear 2-3,040 ft-lb. down, flaps 30', and an airspeed of V +20 knots? 3-3,180 ft-lb. 1-9,800 pounds. 6032. (Refer to figure 94.) Given the following conditions, 2-11,200 pounds. what is the minimum torque for takeoff? 3-17,000 pounds. Pressure altitude 7,500 ft +35° C 6025. (Refer to figure 92.) What thrustisrequired to Temperature (OAT) maintain level flight at 110,000 pounds, with gear down, Ice vanes Retracted flaps 40', and an airspeed of 118 knots. 1-2,820 ft-lb. 1-17,000 pounds. 2-2,880 ft-lb. 1-20,800 pounds. 3-2,780 ft-lb. Z-.-22,300 pounds.

79 69 6033. (Refer to figure 94.) Given the following conditions, 6038. (Refer to figure 95.) Given the following conditions, what is the minimum torque for takeoff? what isthe takeoff distance over a 50-foot obstacle?

Pressure altitude 7,500 ft Pressure altitude 2,000 ft Temperature (OAT) +9° C Temperature (OAT) +15° C Ice vanes Extended Weight 16,800 lb 1-3,200 ft-lb. Wind component Calm 2-3,160 ft-lb. Ice vanes Retracted 3-3,300 ft-lb. 1-3,400 feet. 2-3,700 feet. 6034. (Refer to figure 94.) Given the following conditions, 3-4,200 feet. what is the minimum torque for takeoff? 6039. (Refer to figure 95.) Given the following conditions, Pressure altitude 3,500 ft what is the takeoff ground roll and V1 speed? Temperature (OAT) +43' C Ice vanes Retracted Pressure altitude 3,000 It 1-3,000 ft-lb. Temperature (OAT) -10' C 2-3,050 ft-lb. Weight 15,000 lb 3-3,110 ft-lb. Wind component 8 kts TW Ice vanes Extended 6035. (Refer to figure 94.) Given the following conditions, 1-2,200 feet, 105 knots. what is the minimum torque for takeoff? 2-2,000 feet, 113 knots. Pressure altitude 5,500 ft 3-1,900 feet, 103 knots. Temperature (OAT) +29' C Ice vanes 6040. (Refer to figure 95.) Given the following conditions, Retra ,x1 what is the takeoff distance over a 50-foot obstacle? 1-2,950 ft-lb. 2-3,100 ft-lb. Pressure altitude 6,000 ft 3-3.?00 ft-lb. Temperature (OAT) +35' C Weight 14,500 lb 6036. (Refer to figure 95.) Given the following conditions, Wind component 10 kts HW what is the takeoff distance overa 50-foot obstacle? Ice vanes Retracted 1-4,150 feet. Pressure altitude Sea Level Temperature (OAT) +12' C 2-4,550 feet. Weight 16,000 lb 3-2,600 feet Wind component 16 kts HW 6041. (Refer to figure 96.) Given the following conditions, Ice vanes Retracted what is the accelerate-stop bald length? 1-1,750 feet. 2-2,800 feet. Pressure altitude 5,000 ft 3-2,550 feet. Temperature (OAT) +20' C Weight 15,000 lb 6037. (Refer to figure 95.) Given the following conditions, Win I component 10 kts HW what is the takeoff ground roll and V1 speed? Ice vanes Retracted

Pressure altitude 4,000 ft 1-6,300 feet Temperature (OAT) 0' C 2-4,700 feet. Weight 15,500 lb 3-4,300 feet. Wind component 10 kts TW 6042. (Refer to figure 96.) Given the following conditions, Ice vanes Extended what is the accelerate-stop field length? 1-2,900 feet, 106 knots. 2-4,250 feet, 102 knots. Pressure altitude 2,000 ft 3-2,700 feet, 107 knots. Temperature (OAT) -15' C Weight 16,000 lb Wind component 5 kts TW Ice vanes Extended 1-3,750 feet 2-4,600 feet. 3-4,250 feet. 6043. (Refer to figure 96.) Given the following conditions, 6049. (Refer to figures 97, 98, and 99.) What is the two- what is the accelerate-stop field length? engine rate of climb after takeoff in climb configuration for Operating Condition B-24? Pressure altitude 6,000 ft Temperature (OAT) + 10' C 1-2,100 ft/min. Weight 16,600 lb 2-2,400 ft/min. Wind component 15 kts HW 3-1,500 ft/min. Ice vanes Refracted 6050. (Refer to figures 97, 98, and 99.) What is the single- 1-4,950 feet engine rate of climb after takeoff in climb configuration for 2-4,800 feet Operating Condition B-25? 3-5,300 feet 1-385 ft/min. 6044. (Refer to figure 96.) Given the following conditions, 2-780 ft/min. what is the accelerate-stop field length? 3-665 ft/min. Pressure altitude 8,000 ft 6051. (Refer to figures 97 and 100.) What are the time, Temperature (OAT) -5° C fuel, and distance from the start of climb to cruise altitude Weight 14,000 lb for Operating Condition B-21? Wind component. 4 kts 1W Ice vanes. Extended 1-10.0 minutes; 290 pounds; 35 NAM. 2-10.0 minutes; 165 pounds; 30 NAM. 1-4,500 feet 3-11.5 minutes; 165 pounds; 30 NAM. 2-4,800 feet. 3-5,300 feet 6052. (Refer to figures 97 and 100.) What are the time, fuel, and distance from the start of climb to cruise altitude . (Refer to figure 96.) Given the followingconditions, for Operating Condition B-22? what is the accelerate-stop field length? 1-12.0 minutes; 220 pounds; 40 NAM. Pressure altitude Sea Level 2-11.0 minutes; 185 pounds; 37 NAM. Temperature (OAT) +30' C 3-10.5 rinutes; 175 pounds; 32 NAM. Weight 13,500 lb Wind component 14 kts HW 61153. (Refer to figures 97 and 100.) What are the time, Ice vanes. Refracted fuel, and distance from the start of climb to cruise altitude for Operating Condition B-23? 1-2,500 feet 2-2,850 feet 1-13.0 minutes; 180 pounds; 35 NAM. 3-3,050 feet. 2-14.0 minutes; 210 pounds; 40 NAM. 3-15.0 minutes; 240 pounds; 46 NAM. 6046. (Refer to figures 97, 98, and 99.) What is the two- engine rate of climb after takeoff in climb configuration for 6054. (Refer to figures 97 and 100.) What are the time, Operating Condition B-21? fuel, and distance from the start of climb to cruise altitude for Operating Condition B-24? 1-1,350 ft/min. 2-2,450 ft/min. 1-12.0 minutes; 220 pounds; 45 NAM. 3-2,300 ft/min. 2-9.0 minutes; 185 pounds; 38 NAM. 3-10.0 minutes; 170 pounds; 30 NAM. 6047. (Refer to figures 97, 98, and 99.) What is the single- engine climb gradient after takeoff in climb configuration for 6055. (Refer to figures 97 and 100.) What are the time, Operating Condition 8-22? fuel, and distance from the start of climb to cruise altitude for Operating Condition B-25? 1-6.8 percent gradient 2-7.5 percent gradient 1-11.5 minutes; 170 pounds; 31 NAM. 3-5.6 percent gradient. 2-8.0 minutes; 270 pounds; 28 NAM. 3-12.5 minutes; 195 pounds; 38 NAM. 60411. (Refer to figures 97, 98, and 99.) What is the two- engine rate of climb after takeoff in climb configuration for 6056. (Refer to figures 101 and 103.) At what altitude is the Operating Condition B-23? service ceiling with one engine inoperative for Operating Condition B-26? 1-1,600 ft/min. 2-2,800 ft/min. 1-13,000 feet. 3-2,490 ft/min. 2-14,200 feet. 3-13,600 feet. 6067. (Refer to figures 101 and 103.) Which statement is 6065. (Refer to figures 102, 104, 105, 106, and 118.) What true regarding performance with one engine inoperative for is the en route time of the cruise leg for Operating Operating Condition 8-27? Condition B-35? 1Climb rate at the MEA ismore than 50 ft/min. 1-1 hour 6 minutes. 2Service ceiling is below the MEA. 2-1 hour 8 minutes. 3Bleed air OFF improves service ceiling by 3,000 feet. 3-1 hour 10 minutes.

6038. (Refer to figures 101 and 103.) At what altitude is the 6066. (Refer to figures 102, 104, 105, 106, and 118.) What service ceiling with one engine inoperative for Operating is the fuel consumption during the cruise leg for Operating Condition 8-28? Condition 8-31? 1-1,500 feet above the MEA. 1-812 pounds. 2-10,400 feet. 2-749 pounds. 3-11,800 feet. 3-870 pounds.

6059. (Refer to figures 101 and 103.) Which statement is 6067. (Refer to figures 102, 104, 105, 106, and 118.) What true regarding performance with one engine inoperative for is the fuel consumption during the cruise leg for Operating Operating Condition B-29? Condition B-32? 1 Service ceiling is more than 100 feet above the MEA. 1-1,028 pounds. 2Bleed air must be off to obtain a rate of climb of 2-896 pounds. 50 ft/min at the MEA. 3-977 pounds. 3Climb is not possible at the MEA. 6068. (Refer to figures 102, 104, 105, 106, and 118.) What 6060. (Refer to figures 101 and 103.) At what altitude is the is the fuel consumption during the cruise leg for Operating service ceiling with one engine inoperative for Operating Condition B-33? Condition B40? 1-1,165 pounds. 1-9,800 feet 2-1,373 pounds. 2-13,200 feet 3-976 pounds. 3-2,100 feet above the MEA. 6069. (Refer to figures 102, 104, 105, 106, and 118.) What 6061. (Refer to figures 102, 104, 105, 106, and 118.) What is the fuel consumption during the cruise leg for Operating is the en route time of the cruise legfor Operating .condition B-34? Condition 8-31? 1-668 pounds. 1-1 hour 11 minutes. 2-718 pounds. 2-1 hour 17 minutes. 3-737 pounds. 3-1 hour 19 minutes. 6070. (Refer to figures 102, 104, 105, 106, and 118.) What 6062. (Refer to figures 1u2, 104, 105, 106, and 118.) What is the fuel consumption during the cruise leg for Operating is the en route time of the cruiselegfor Operating Condition B-35? Condition 8-32? 1-900 pounds. 1-1 hour 13 minutes. 2-1,030 pounds. 2-1 hour 15 minutes. 3-954 pounds. 3-1 hour 20 minutes. 6071. (Refer to figure 107.) What are the time and distance 6063. (Refer to figures 102, 104, 105, 106. and 118.) What to descend from 18,000 feet to 2,500 feet? is the en route timeof the cruiselegfor Operating Condition B-33? 1-10.3 minutes, 39 NAM. 2-9.8 minutes, 33 NAM. 1-1 hour 50 minutes. 3-10.0 minutes, 36 NAM. 2-1 hour 38 minutes. 3-1 hour 48 minutes. 6072. (Refer to figure 107.) What are the distance and fuel consumption to descend from 22,000 feet to 4,500 feet? 6064. (Refer to figures 102, 104, 105, 106, and 118.) What isthe en route time of the cruiselegfor Operating 1-44 NAM, 117 pounds. Condition 844? 2-48 NAM, 112 pounds. 3 -56 NAM, 125 pounds. 1-1 hour 6 minutes. 2-1 hour 3 minutes. 6073. (Refer to figure 107.) What are the time and distance 3-1 hour 11 minutes. to descend from 16,500 feet to 3,500 feet? 1-9.3 minutes, 37 NAM. 2-9.1 minutes, 35 NAM. 3-8.7 minutes, 33 NAM.

8272 6074. (Refer to figure 107.) What are the distance and fuel 608^ (Refer to figures 108 and 109.) What is the remaining consumption to descend from 13,500 feet to 1,500 feet? runt/ length when stopped after landing over a 50-foot °bats,for Operating Condi Ion B-39? 1-30 NAM, 87 pounds. 2-29 NAM, P1 pounds. 1-2,300 feet. 3-38 NAM, 100 pounds. 2-2,400 feet. 3-2,500 feet. 6075. (Refer to figure 107.) What are the time and distance to descend from 23,000 feet to 800 feet with an average 6083. (Refer to figures108 and109.) What are the 15-knot headwind? approach speed and groundroll when landing under Operating Condition B-3? 1-14.2 dilutes, 50 miles. 2-14.6 minutes, 58 miles. 1-111 knots and 1,550 feet. 3-14.9 n mutes, 59 miles. 2-110 knots and 1,400 feet 3-109 knots and 1,300 feet 6076. (Refer to figures 108 and 109.) What is the landing distance overa 50-foot obstacle for Operating 6084. (Refer to figures 108 and 109.) What is the landing Condition 8-36? distance over a 50-fuot obstacle for Operating Condition 8-40? 1-1,900 feet 2-1,825 feet 1-1,500 feet 3-950 feet 2-1,750 feet 3-1,650 feet 6077. (Refer to figures 108 and 109.) What are the approach speed and groundroll when landing under 6085. (Refer to figures 108 and 109.) What is the total Operating Condition B-36? runway used when touching down at the 1,000-foot marker :or Operating Condition B-40? 1-113 knots and 950 feet 2-113 knots and 1,950 feet 1-1,800 feet 3-112 knots and 900 feet 2-1,650 feet. 3-1,550 feet 8078. (Refer to figures 108 and 109.) What is the remaining runway length when stopped after landing over a 50-foot 6086. (Refer to figure 110.) Given the following conditions, obstacle for Operating Condition B-37? what is the maximum allowable rgesured gas temperature (MGT) during the power assurance check? 1-2,500 feet 2-2,000 feet Engine torque 57 percent 3-Z600 feet Pressure altitude 2,500 ft Temperature (OAT) +5' C 6076. (Refer to figures106 and 109.) What are the approach speed and ground roll when landing under 1-810' C. Operating Condition B-37. 2-815' C. 3-828' C. 1-108 knots and 1,400 feet 2-109 knots and 900 feet. 6087. (Refe to figure 110.) Given the following conditions 3-107 knots a xi 1,350 feet is the maximum allowable measured gas temperature (MGT) durins the power assurance check? 6060. (Refer to figures 108 and 109.) What is the landing distance over a 50-foot obstacle for Operating Engine torque 49 percent Condition B-38? Pressure altinde 5,500 ft Temperature (OAT) +25' C 1-t850 feet 2-1,700 feet 1-870' C. 3-1,800 feet 2-855' C. 3-880' C. 6061. (Refer to rigures 108 and 1094 Wha! Is the total runway used when touchdown is a* the 1"00 -foot marker 6088. (Refer to figure 110.) Given the following conditions, for Operating Condition B-38? what Is the maximum allowable measured gas temperature (MGT) during the power assurance c. neck? 1-2,000 feet 2-1,700 feet Engine torque 54 percent 3-1,800 feet Pressure attitude 500 ft roperature (OAT) +256 C 1-840' C. 2-830' C. 3-820' C. 60119. (Refer to figure 110.) Given the following conditions, 6096. (Refer to figure 112.) What is the maximum gross what is the maximum allowable measuredgas temperature weight for hovering out of ground effect at 3,000 feet (MGT) during the power assurance check? pressure altitude and +30' C? Engine torque 43 percent 1-17,500 pounds. Pressure altitude 9,000 ft 2-14,300 pounds. Temperature (OAT) -15' C 3-13,400 pounds. 1-782' C. 2 -768' C. 6097. (Refer to figure 112.) What is the maximum gross 3-750' C. weight for hovering ow of ground effect at 6,000 feet pressure altitude and + ' C? 6090. (Refer to figure 110.) Given the following conditions, 1-16,800 pounds. what is the maximum allowable measuredgas temperature 2-13,500 pounds. (MGT) during the power assurance check? 3-14,400 pounds. Engine torque 52 percent 6098. (Refer to figure 112.) What is the maximum, nes Pressure altitude 1,500 ft weight for hovering out of ground effect at 7,000 :set Temperature (OAT) +35' C pressure altitude and +35' C? 1-880' C. 1-14,000 pounds. 2-885' C. 2- 11,600 pounds. 3-872* C. 3-12,500 pounds. 0091. (Refer to figure 111.) What is the maximum gross 6099. (Refer to figure 112.) What is the maximum gross weight for hovering in ground effect at 3,000 feetpressure weight for hovering out of ground effect at 4,500 feet altitude and +25' C? pressure altitude and +20' C? 1-17,300 pounds. 1-14,500 pounds. 2-14,700 pounds. 2-14,000 pounds. 3-18,000 pounds. 3-17,000 pounds. GOO. (Refer to figure 111.) What is the maximum gross 6100. (Refer to figure 112.) What is the maximum gross weight for hovering in ground effect at 6,000 feetpressure altitude and +15' C? weight for hovering out of ground effect at 2,500 feet pressure altitude and + 30' C? 1-17,200 pounds. 1-17,400 pounds. 2-16,800 pounds. 2-15,000 pounds. 3-14,200 pounds. 3-14,500 pounds. OM (Refer to figure 111.) What is the maximum gross 6101. (Refer to figure 113.) Given the following, what is the weight for ;layering in ground effect at 7,000 feet pressure takeoff distance over a 50-foot obstacle? altitude and +35' C? Pressure altitude 1-1S,a00 pounds. 3,500 ft Temperature (OAT) 2-14,700 pounds. +20' C Gross weight 3-12,100 pounds. 15,000 lb 1-1,070 feet. MK (Refer to figure 111.) What is the maximumgross 2-1,020 feet weight for hovering in ground effect at 4,500 feetpressure 3-1,100 feet altitude and +20' C? 1-14,500 pounds. 6102. (Refer to figure 113.) Given the following, what is the takeoff distance over a 50foot obstacle? 2-18,500 pounds 3- -17,000 pounds. Pressure altitude 6,000 ft Temperature (OAT) C 6095. (Refer to figure 111.) What is the maximumgross Gross weight 11,000 lb weight for hovering in ground effect at 2,500 feetpressure altitude and +35' C? 1-1,000 feet 2-920 fe^ 1-18,200 pounds. 3-870 feet 2-16,000 pounds, 3-14,800 pow&

8474 6103. (Refer to figure 1'1.) Given the following, what is the 8109. (Refer to figure 114.) Given the following, what is the takeoff distance over a 50-foot obstacle? climb performance with both engines operating?

Pressure altitude 6,500 ft Pressure altitude 11,500 ft Temperature (OAT) 0' C Temperature (OAT) -15° C Gross weight 13,500 lb Heater ON 1-1,500 feet. 1-645 ft/min. 2-1,050 feet. 2-375 ft/min. 3-1,100 feet 3-330 ft/min.

6104. (Refer to figure 113.) Given the following, what is the 6110. (Refer to figure 114.) Given the following, what is the takeoff distance over a 50-foot obstacle? climb performance with both engines operating? Proems altitude 9,000 ft Pressure attitude 3,500 ft Temperature (OAT) +20' C Temperature (OAT) -10' C Gross weight 15,000 lb Heater ON 1-1,300 feet 1-985 ft/min. 2-1,350 feet 2-1,300 ft/min. 3-1,250 feet 3-1,360 ft/min.

6106. (Refer to figure 113.) Given the following, what is the 61 i1. (Refer to figure 115.) Given the following, what is the takeoff distance over a 50-foot obstacle? single-engine climb or descent performance?

Pressure altitude -1,000 ft Pressure altitude 7,500 ft Temperature (OAT) +25' C Temperature (OAT) 0' C Gross weight 14,000 lb 1-80 ft/min descent 1-1,000 feet 2-10 ft/min ciimb. 2-900 feet 3-50 ft/min climb. 3-950 feet 6112. (Refer to figure 115.) Given the following, what is the 6106. (Refer to figure 114.) Given the following, what is the single-engine climb or descent performance? climb performance with both engines operating? Pressure altitude 3,000 ft Pressure altitude 9,500 ft Temperature (OAT) +35' C Temperature (OAT) -5' C 1-150 ft/min descent Heater "4 2-350 ft/min climb. 1-925 ft/min. 3-100 ft/min descent 2-600 ft/mkt 3-335 ft/min. 6113. (Refer to figure 115.) Given the following, what is the single-engine climb or descent performance? 6107. (Refer to figure 114.) Given the following, what is the 4,700 ft climb performance with both engines operating? Pressure altitude Temperature (OAT) +20' C Pressure altitude 7,500 ft emperature (OAT) +5' C 1-420 ft/min climb. Heater ON 2-80 ft/min climb. 3-60 ft/lain decent 1-905 ft/min. 2-765 ftimin. 6114. (Refer to figures 115.) Given the following, what is 3 -1,080 ft/min. the single-engine climb or descent performance? Pressure altitude 9,500 ft 6106. (Refer to figure 114.) Given the following, what is the -10' C climb performance with both engines operating? Temperature (OAT) 1-600 ft/min descent Pressure altitude 8,500 ft 2-840 ft/rnin descent. Temperature (OAT) +25' C Heater OFF 3-280 ft/min descent. 1-285 ft/mkt. 2-800 ft/min. 3-400 ft/min.

76 6115. (Refer to figure 115.) Given the following, what is the 6121. (Refer to figure 117.) Given the following, what is the single-engine climb or descent performance? single-engine landing distance over a 50-foot obstacle?

Pressure altitude 1,500 ft Gross weight 12,000 lb Temperature (OAT) +45' C Pressure Altitude 3,500 ft 1-100 ft/min descent. Temperature (OAT) +30° C 2-360 ft/min climb. 1-850 feet. 3-200 ft/min descent 2-900 feet. 3-1,000 feet. 6116. (Refer to figure 118.) Given the following, what is the airspeed limit (VN1)? 6122. (Refer to figure 117.) Given the following, what is the single-engine landing distance over a 50-foot obstacle? Gross weight 16,500 lb Pressure altitude 5,000 ft Gross weight 16,500 lb Temperature (OAT) -15° C Pressure altitude 5,500 ft 1-128 KIAS. Temperature (OAT) -10° C 2-133 KIAS. 1-1,700 feet. 3-126 KIAS. 2-1,550 feet. 3-1,600 feet. 6117. (Refer to figure 116.) Given the following, what is the airspeed limit (VN1)? 6123. (Refer to figure 117.) Given the following, what is the single-engine landing distance over a 50-foot obstacle? Gross weight 17,500 lb Pressure altitude 4,000 ft Gross weight 15,000 6 Temperature (OAT) +10° C Pressure altitude 8,000 ft 1-114 KIAS. Temperature (OAT) +20° C 2-120 KIAS. 1-1,900 feet. 3-130 KIAS. 2-1,800 feet. 3-2,000 feet. 6118. (Ref, lure 116.) Given the following, what is the airspeed lir ? 6124. (Refer to figure 117.) Given the following, what is the single-engine landing distance over a 50-foot obstacle? Gross weir 15,000 lb Pressure t 6,000 ft Gross weight 14,000 lb Temperas ) 0° C Pressure altitude 1,000 ft 1-135 K Temperature (OAT) +10° C 2-127 lk. 1-650 feet. 3-143 KIA,. 2-720 feet 3-800 feet. 6119. (Reiter to figure 116.) Given the following, what is the airspeed limit (V14)? 612F,. (Reiss to figure 117.) Given the following, what is the sinjle-engine anding distance over a 50-foot obstacle? Grossweight 14,000 lb Pressure altitude 8,000 ft Gross weight 17,000 lb Temperature (OAT) -15' C Pressure altitude 4,000 ft 1-121 KIAS. Temperature (OAT) +40° C 2-123 KIAS. 1-1,850 feet. 3-113 KIAS. 2-2,200 feet. 3-2,000 feet 6120. (Refer to figure 116.) Given the following, what is the airspeed limit (V14)? 6126. Under which conditions is hydroplaning most likely to occur? Gross weight 12,500 lb Pressure altitude 14,000 ft 1 -When a landing is made at minimum landing speed with Temperature (OAT) -20° C an abrupt initial runway contact during heavy precipita- 1-99 KIAS. tion. 2-108 KIAS. 2-During conditions of standing water, slush, high speed, 3-103 KIAS. and smooth runway texture. 3-During a landing on any wat runway when brake application is delayed until a wedge of water begins to build ahead of the tires.

78 6127. What effect,if any, will landing at a higher-than- 6136. At what minimum speed will dynamic hydroplaning recommended touchdown speed have on hydroplaning? begin if a tire has an air pressure of 80 PSI? 1No effect on hydroplaning, but increases landing roll. 1-80 knots. 2Reduces hydroplaning potentialifheavy brakingis 0-86 knots. agile& 3-92 knots. 3Increases hyaroplaning potential regardless of braking. 6137. Which flight conditions of a large jet airplane create 6128. A takeoff is not recommended ifstanding water, the most severe flight hazard by generating wingtip vortices slush, or wet snow on the runway is more than what of the greatest strength? maximum depth? 1Heavy, slow, gear and flaps up. 1-1/4 inch. 2Heavy, slow, gear and flaps down. 2-1/2 inch. 3Heavy, fast, gear and flaps down. 3-1 inch. 6138. Hazardous vt.rtex turbulence that might be encoun- 6129. What is the best method of speed reductionif tered behind large aircraft is created only when that aircraft hydroplaning is experienced on landing? is 1Apply full main wheel braking only. 1developing lift. 2Apply nosewheel and main wheel braking alternately and 2operating at high airspeeds. abruptly. 3using high power settings. 3Apply aerodynamic 1.-:aking to the fullest advantage. 6139. Wingtip vortices created by large aircraft tend to 6130. Compared to dynamic hydroplaning, at what speed does viscous hydroplaning occur when landing on a smooth, 1sink below theaircraftgeneratingtheturbulence. wet runway? 2rise from the surface to traffic pattern altitude. 3accumulate and remain for a period of time at the point 1At approximately 2.0 times the speed that dynamic where the takeoff roll began. hydroplaning occurs. 2At a lower speed than dynamic hydroplaning. 6140. How does the wake turbulence vortex circulate 3At the same speed as dynamic hydroplaning. around each wingtip?

6131. What term is used to describe hydrople. .ng which 1Inward, upward, and around the wingtip. occurs when an airplane's tire is held off a smooth runway 2Counterclockwise when viewed from behind the aircraft. by steam generated from the heat of friction? 3outward, upward, and around the w;rigfI. 1Reverted rubber hydroplaning. 6141. Which statementistrueconcerningthe wake 2Dynamic hydroplaning. turbulence produced by a large transport aircraft? 3Viscous hydroplaning. 1Vortices can be avoided by flying 300 feet below and 6132. At what minimum speed will dynamic hydroplaning behind the flightpath of the generating aircraft begin if a tire has an air pressure of 70 PSI? 2The vortex characteristics of any given aircraft may be altered by extending the flaps or changing the speed. 1--85 knots 3Wake turbulence behind a propeller-driv in aircraft is 2-80 knots. negligible because jet engine thrust is a necessary factor 3-75 knots. in the formation of vortices.

6133. At what minimum speed will dynamic hydroplaning 6142. What effect would a light crosswind have on the begin if a tire has an air pressure of 90 PSI? wingtip vortices generated by a large airplane that has just taken off? 1-85 knots. 2-88 knots. 1The upwind vortex will tend to remain on the runway 3-90 knots. longer than the downwind vortex. 2A crosswind will rapidly dissipate the strength of both 6134. At what minimum speed will dynamic hydroplaning rirtices. begin if a tire has an air pressure of 110 PSI? 3The downwind vortex will tend to remain on the runway 1-103 knots. longer than the upwind vortex. 2-96 knots. 6143. To avoid the wingtip vortices of a departing Jet 3-94 knots. airplane during takeoff, the pilot should 6136. At what minimum speed will dynamic hydroplaning 1lift off at a point well past the jet airplane's flightpath. begin if a tire has an air pressure of 95 PSI? 2climb above a xi stay upwind of the jet airplane's 1-80 knots. flightpath. 2-68 knots. 3-- remain below the flightpath of the jet airplane. 3-00 knots.

77 Ere 6144. What wind condition prolongs the hazards of wake 6152. (Refer to figure 119.) When penetrating a microburst, turbulence on a landing runway for the longest period of which aircraft will experience an increase in performance time? without a change in pitch or power? 1Direct tailwind. 1-3. 2Light quartering tailwind. 2-2. 3Light quartering heaowind. 3-1.

6145. If you take off behind a heavy jet that has just 6153. (Refer to figure 119.) The aircraft in position 3 will landed, you should plan to lift off experience which effect in a microburst encounter? 1prior tothepoint where thejettouched down. 1Decreasing headwind. 2beyond the point where the jet touched down. 2Increasing tailwind. 3at the point where the jet touched down andon the 3--Strong downdraft upwind edge of the runway. 6154. (Refer to figure 119.) What effect will a microburst 6146. What action is appropriate when encountering the encounter have upon the aircraft in position 4? first ripple of reported clear air turbulence? 1Strong tailwind. 1Extend flaps to decrease wing loading. 2Strong updraft 2Extend gear to provide more drag and increase stability. 3Significant performance increase. 3Adjust airspeed to that recommended for rough air. 6155. (Refer to figure119.) How willtheaircraftin 6147. If severe turbulence is encountered which procedure position 4 be affected by a microburst encounter? is recommended? 1Performance increasing with a tailwind and updraft 1Maintain a constant altitude. 2Performance decreasing with a tailwind and downdraft 2Maintain a constant attitude. 3Performance decreasing with a headwind and downdraft. 3Maintain constant airspeed and altitude. 6156. Which cockpit indications occur when a constant 6148. What isthe expected duration of an individual tailwind component shears to a calm wind? microburst? 1Altitude increases; pitch and indicated airspeed de- 1Five minutes with maximum winds lasting approximately crease. 2-4 minutes. 2Altitude, pitch, and indicated airspeed increase. 2One microburst may continue for as longas an hour. 3Altitude decreases; pitch and indicated airspeed in- 3Seldom longer than 15 minutes from the time the burst crease. strikes the ground until dissipation. 6157. What effect will a change in 'wind direction have upon 6149. Maximum downdrafts in a microburst encountermay maintaining a 3' glide slope a: a constant true airspeed? be as strong as 1When groundspeed decreases, rate of descent must 1-1,500 feet per minute. increase. 2-4,500 feet per minute. 2When groundspeed increases, rate of descent must 3-8,000 feet per minute. increase. 3Rate of descent must be constant to remain on tne glide 6150 An aircraft that encounters a headwind of 40 knots, slope within a microburst, may expect a total shearacross the microburst of 61511. When passing through an abrupt wind shear which 1-40 knots. Involves a shift from a tailwind to a headwind, what power 2-80 knots. management would normally be required to maintain a 3-90 knots. constant indicated airspeed and remain on the ILS glide slope? 6151. (Refer to figure 119.) If involved in a microburst 1Lower-than-normal power initially, followed by a further encounter between which aircraft positions will the most decrease as the wind shear is encountered, then an severe downdraft occur? increase. 1-4 and 5. 2Higher-than-normal power initially, followed by a de- 2-3 and 4. crease as the shear is encountered, then an increase. 3-2 and 3. 3Lower-than-normal power initially, followed by an In- crease as the shear is encountered, then a decrease.

at 78 6159. While flying an ILS glide slope, a constant taihvind 6167. How should thrust reversers be applied to reduce sheers to a calm wind. Which conditions should the pilot landing distance for turbojet aircraft? expect? 1Immediately after ground contact 1Airspeed and pitch attitude decrease, and a tendency to 2 Immediately prior to touchdown. go below the glide slope. 3After applying maximum wheel braking. 2Airspeed and Ott attitude increase, and a tendency h. go above 0*. z, glide slope. 6166. Throughoutthelandingroll,whatisthe most 3Airspeer and pitch attitude decrease, and a tendency to effective method of deceleration regardless of runway go above' the glide slope. surface?

81110 While flying in ILS glide slope, a headwind shears to 1Application of aerodynamic drag devices. a tailwind. Which conditions should thepilotexpect? 2Continuous use of thrust reversers. 3Judicious use of wheel brakes. 1Airspeed and pitch attitude decrease, and a tendency to go below the glide slope. 8169. During the takeoff roll, which factor decreases as 2Airspeed and pitch attitude increase, and a tendency to airspeed increases? go above the glide slope. 3Airspeed and pitch attitude decrease, and a tendency to 1Aerodynamic drag. go above the glide slope. 2Rolling friction. 3Coefficient of lift. 61111. During an en route descent in a fixed thrust and 6170. Which condition reduces the required runway for N. fbad-pitth attitude ,:onfiguration, both the ram air input and drain hole of the pitot system become completely blocked Takeoff? by ica What airspeed indication can be expeced? 1Higher-than-recommended airspeed before rotation. 1increase in indicated airspeed. 2Lower-than-standard air density. 2 Decrease In indicated airspeed. 3Increased headwind component 3Indicated airspeed remains at the value prior to icing. 6171. Which performance factor decreases as airplane 8162. What can a pilot expect if the pitot system ram air gross weight increases? input and drain hole are blocked by ice? 1Critical engine failure speed. 2Rotation speed. 1The airspeedindicator may act as analtimeter. 3Accelerate-stop distance. 2The airspeed indicritor will show a decrease withan increase in altitude. 6172. Maximum range performance of a turbojet aircraft is 3No airspeed indicator change will occur during climbs or obtained by which procedure as aircraft weight reduces? descants. 1 Increasing speed or altitude. 6101. If both the ram air input and drain hole of the pitot 2Increasing altitude or decreasing goad. system are blocked by ice, what airspeed indication can be 3Increasing speed or decreasing altitude. expected? en& Which procedure produces the minimum fuel con- 1No variation of indicated airspeed in level flight if large sumption fix a given leg of the cruise flight? power changes are made. 2Decrease of indicated airspeed during a climb. 1Increase speed for a headwind. 3 Constant indicated airspeed during a descent. 2Increase speed for a tailwind. 3Increase altitude for a headwind, decrease altitude for a 6154. What effect does an uphill runway slope haveupon tailwind. takeoff performance? 6174. How should reverse thrust propellers be used during 1 Increases takeoff distance. landing for maximum effectiveness in stopping? ' Decreases takeoff speed. 3Decreases takeoff distance. 1Gradually increase reverse power to maximum as rollout speed decreases. 61I5. Under which condition during the landing roll are the 2Use maximum reverse power as soon as possible after main wheel brakes at maximum effectiveness? couchdovm. 1When wing lift has been reduced. 3Select reverse-pitch after landing and use Idle power 2At high groundspeed.. setting of the engikes. 3When the wheels are locked and skidding. 8175. To obtain optimum range conditions in a turbojet SIN. Which condition has the effect of I educing critical airplane, cruising Mg ht should be planned engine failure speed? 1at any altitude within the troposphere. 1Sluth on the runway or inoperative antiskid. 2at, or above the tropopause. 2Las gross might. 3at any altitude above the jetstream level. 11Rgh density altitude.

79 es 6176. Which place in the turbojet engine Is subjected to the 6184. Which type of compressor stall has the greatest highest temperature? potential for severe engine damage? 1Compressor discharge. 1Intermittent "backfire" stall. 2Fuel spray nozzles. 2Transient "backfire" stall. 3Turbine inlet. 3Steady, continuous flow reversal stall.

6177. What effect would a change in ambient temperature 6185. What recovery would be appropriate in the event of or air density have on gas-turbine-engine performance? compressor stall?

1As air density decreases, thrust increases. 1Reduce fuel flow, reduce angle of attack, andincrease 2As temperature increases, thrust increases. airspeed. 3As temperature increases, thrust decreases. 2Advance throttle, lower angle of attack, and reduce airspeed. 6178. The most important restriction to the operation of 3Reduce throttle, reduce airspeed, and increase angle of turbojet or turboprop engines is attack. 1limiting compressor speed. 2limiting exhaust gas temperature. 6186. Under normal operating conditions, which combination of MAP and RPM produce the most severe wear, 3 torque. fatigue, and damage to high performance reciprocating 6179. As outside air pressure decreases, thrust output will engines? 1inaease due to greater efficiency of jet aircraft in thin 1High RPM and low MAP. air. 2Low RPM and high MAP. 2remain the same since compression of inlet air will 3High RPM and high MAP. compensate for any decrease in air pressure. 3 decrease due to higher density altitude. 61117. What effect does high relative humidity have upon the maximum power output of modem aircraft engines? 6180. What effect will an increase in altitude haveupon the 1Neither turbojet or reciprocating engines are affected. available equivalent shaft horsepower (ESHP) ofa turboprop 2Reciprocating engines will experience a significant loss engine? of BHP. 1Lower air density and engine mass flow willcause a 3Turbojet engines will experience a significant loss of decrease in power. thrust 2Higher propeller efficiency will causean increase in usable power (ESHP) and thrust 6188. Equivalent shaft horsepower (ESHP) of a turboprop engine is a measure of 3Power will remain the same but propeller efficiencywill decrease. 1turbine inlet temperature. 2shaft horsepower and jet thrust. 61111. What effect, if any, does high ambient temperature 3propeller thrust only. have upon the thrust output of a turbine engine?

1Thrust will be reduced due :,% the decrease in air density. 6189. Minimum specific fuel consumption of the turboprop engineisnormallyavailableinwhich altitude range? 2Thrust will remain the same, but turbine temperaturewill be higher. 1-10,000 feet to 25,000 feet 3Thrust will be higher because more heatenergy is 2-25,000 feet to the tropopause. extracted from the hotter air. 3The tropopause to 45,000 feet 6182. What characterizes a transient compressor stall? 6190. Where is the critical altitude of a supercharged- 1Loud, steady roar accompanied by heavy shuddering. reciprocating engine? 2Sudden loss of thrust accompanied bya loud whine. 1The highestaltitudeat which a desiredmanifold 3 Inter ittent "bang," as backfires and flow reversalstake pressure can be obtained. place. 2Highest altitude where the mixture can be leaned to best power ratio. 616$. What indicates that a cc mpressor stall has developed 3 -The altitude at which maximum allowable MEP can be and become steady? obtained. 1Strong vibrations and loud roar. 6191. What 2Oocasional loud "bang" and flow reversal. iscontrolledbythewaste ca ofa turbocharged-reciprocating engine? 3Complete loss of power with severe reductionin airspeed. 1Supercharger gear ratio. 2Exhaust gas discharge. 3Throttle opening.

90 80 6192. How is manual lean (best economy) cruising mixture 6201. What isthe effect of alcohol consumption on setting obtained on a large, supercharged, reciprocating functions of the body? engine? 1 Alcohol has an adverse effect, especially as altitude 1Lean to best power BMEP, then enrichen a specific RPM increases. drop. 2Small amounts of alcohol in the human system increase 2Lean to the detonation point, then enrichen a specific judgment and decision-making abilities. BMEP rise. 3Alcohol has little effect if followed by equal quantities of 3Lean to best power BMEP, then lean to a specific BMEP black coffee. drop. 6202. A pilot is more subject to spatial disorientation when 6193. What occurs when operating above 35,000 feet in the event of a complete cabin pressure loss? 1ignoring or overcoming the sensations of muscles and inner ear. 1The oxygen pressurewithinthelungs cannot be 2eyes are moved often in the process of cross-checking maintained without a positive increase of inhaled oxygen the flight instruments. pressure. 3body sensations are used to interpret flight attitudes. 2Vision improves significantly as cabin altitude increases because carbon dioxideis released from the body. 6203. Which procedure is recommended to prevent or 3--Gases trapped in the body contract and prevent nitrogen overcome spatial disorientation? from escaping the bloodstream. 1 R educe head and eye movement tothe greatest 6194. What is a symptom of carbon monoxide poisoning? possible extent. 2Rely on the kinesthetic sense. 1Rapid, shallow breathing. 3Rely entirely on the indications of the flight instruments. 2Pain and cramping of the hands and feet. 3Dizzlness. 6204. What is the most effective way to use the vies during night flight? 6196. Which wouki most likely remit in hyperventilation? 1Look only at far away, dim lights. 1A stressful situation causing anxiety. 2Scan slowly to permit off center viewing. 2The excessive consumption of alcohol. 3Concentrate directly on each object for a few seconds. 3An extremely slow rate of breathing and insufficient oxygen. 6206. Microbursts are small-scale intense downdrafts which

6196. What causes hypoxia? 1are easily detected visually due to their association with heavy rain showers. 1--r_xcessive carbon dioxide in the atmosphere. 2dissipate prior to reaching the surface when the wind 2An increase in nitrogen content of the air at high gradient is positive. altitudes. 3upon reaching thesurface,spread outward inall 3A decrease of oxygen partial pressure. directions.

6197. Which is a common symptom of hyperventilation? 6206. The illusion of being in a noseup attitude which may occur during a rapid acceleration takeoffis known as 1TIngling of the hands, legs, and feet 2increased vision keenness. 1inversion illusion. 3Decreased breathing rate. 2 autokinesis. 3somatogravic illusion. 6196. Loss of cabin pressure may result in hypoxia because as cabin altitude increases 6207. In the dark, a stationary light will appear to move when stared at for a period of time. This illusion is known as 1 the percentage of nitrogen in the air is increased. 2the percentage of Jxygen in the airis decreased 1somatogravic illusion. 3oxygen partial pressure is dec. eased. 2ground lighting illusion. 3 autokinesis. 6199. Hypoxia is the result cf which of these conditions? 6206. When making a landing over darkened or featureless 1Insufficient oxygen reaching the brain. terrain such as water or snow, a pilot should be aware of 2Excessive carbon dioxide In the bloodstream. the possibility of illusion. The approach may appear to be 3UmIted oxygen reaching the heart muscles. too 6200. Rapid or extra deep breathing can cause a condition 1 hig h. known as 2low. 1hyprecia. 3shallow. 2vertigo 3hyperventilation.

81 6206. When making an approach to a narrower- than -usual 4216. Which activity is not considered to be form of runway, without VASI assistance, the pilot should be aware "holding out"? that the approach 1Word-of-mouth information that charter flight services 1altitude may be higher than it appears. are continuously available. 2altitude may be lower than it appears. 2Full-time employment as pilot of a company-owned 3may result in leveling off too high and landing hard. aircraft 3Posting a schedule of available charter flight services in 6210. While making prolonged constant rate turns under a fixed-base operator's pilot lounge. IFR conditions, an abrupt head movementcan create the Illusion of rotation on an entirely different axis. This is known 6217. Which term describes a type of private carrier? as 1Contract carder. 1autokinesis. 2Restricted commercial carrier. 2Coriolis illusion. 3Common carder. 3the leans. 6218. Which statement best describes the term "holding 6211. Which observed target aircraft would be of most out"? concern with respect to collision avoidance? 1Offers to the public:the carriage of persons or property 1One which appears to be ahead and moving from leftto for hire, either intrastate or interstate. right at MO Weed. 2Carriage of persons or property for hire for a few 2One which appears to be ahead and moving from right selected customers on an intrastate basis. to left at slow speed. 3Carriage of ,:ergo for an industrial firm on an intrastate 3One which appears to be ahead withno lateral or basis. vertical movement and is increasing in size. 6219. Which is the key factor that determines that an 6212. Scanning procedures for effective collision avoidance of o common carrier rather than a private carrier? should constitute 1Engaging In intrastate carriage of persons or property. 1looking outside for 15 seconds, then inside for 5sec- 2Expression of willingnew to carry all customers. onds, then repeat. 3Engaging In a limited operation of the intrastate carriage 2-1 minuteinsidescanning,then 1 minuto outside of manufactured components for one company. scanning, then repeat 3looking outside every 10 seconds except inradar 6220. An operator who occasionally refuses to transport contact when outside scanning is unnecessary. persons or property, and who holds out on an informal basis, 6213. When using the Earth's horizon asa reference point to determine the relative position of other aircraft,most 1may be considered to meet the criteria for common concern would be for aircraft carriage. 2may be considered a common carrier onlyifthe 1above the horizon and increasing in size. transportationof persons or propertyisinterstate. 2on the horizon with little relative movement 3is a private carrier unless operating undera ("tract 3on the horizon and increasing in size. charter, or mail agreement 6214. Where should a non-ambulatory handicappedpas- 6221. An aircraft configured for air ambulance operations senger be seated to expeditiously accomplish emergency should include evacuation? 1four-point floor anchor points and approved web-type 1At the beginning of a line of passengers that wouldbe restraints for securing stretchers. evacuated through an overwing exit. 2a seat near the patient for an attendant 2New the beginning co. a line of passengers that would be 3a nitrous oxide supply and breathing mask for in-flight evacuated through a ma;ri exit. patient sedation. 3Near the end of a line of passengers that would be evacuated through * floor-level,non- overwingexit 6222. Which is a factor that tends to establish an operator as a private carrier? 6215. An ambulatory handicappedpassenger should be seated in an area where emergency evacuationcan be 1Charter flying for only one orgarization although flights accomplished through are open to the public. 2Carriage of selected customers on a long-term basis 1the aft normal or emergency exit. where no holding out 141 involved. 2an eventing exit. 3Making known publicly, through reputation (not advertis- 3a floor-level exit. ing), that all customers will be provided transportation service.

/ 2 82 6223. A carrier which offers transportation pursuant to 6231. Where is a -nonlocationfor an inversion? separately negotiated contracts, and is holding out by reputation only, 1At the tropopausc 2In the stratosphere. 1is engaged in private carriage whether operations are 3At the base of cumulus clouds. intrastate or interstate. 2may be classified as a common carrier. 6232. The most frequent type of ground- or surface-based 3meets the criteria of private carriage if the contracts temperature inversion is produced by stipulate interstate operations. 1the movement of colder air under warm air, or the 6224. An intrastate commercial operator meets the criteria movement of warm air over cold air. that has been established for a common carrierifit 2widespread sinking of air within a thick layer aloft resulting in heating by compression. 1carries only emp'oyees of one corporation for hire within 3terrestrial radiation on a clear, relatively calm night the boundaries of one state, on a long-term basis. 2does not hold out transportation service to the public 6233. Which term applies when the temperature of the air and operates with very few contracts. changes by compression or expansion with no heat added 3offers to carry manufactured components under 15 indi- or removed? vidual contracts on interstai a flights. 1Katabatic. 6225. On a number of occasions an operator makes verbal 2Advection. of to senior citizens' groups to transport them in his 3Adiabatic. aircraft to a casino located in another state. This operator 6234. Unsaturated air flowing upslope will cool at the rate would be considered to be of about 1a common carrier if compensation is received from the 1-3' C per 1,000 feet. passenger& 2-26 C per 1,000 feet 2a private carrier because there is no published hoidinr 3e C per 1,000 feet out of services. 3engaged in common carriage if the trip generates a profit 6235. If the ambient temperature is warmer than sten -14rd and private carriage if no profit is realized. at FL350, what is the density altitude compared to pressure altitude? UK What is a characteristic of the troposphere? 1Lower than pressure altitude. 1it contains all the moisture of the atmosphere. 2There is an overall decrease of temperature with an 2Higher than pressure altitude. increase of altitude. 3Impossible to determine without information on possible 3The average altitude of the top of the troposphere is inversion layers at lower altitudes. about 6 miles. 6236. If the ambient temperature is colder than standard at 6227. The primary cause of all changes in the Earth's FL310, what is the relationship between true altitude and pressure altitude? weather is 1They are both the same, 31,000 feet 1 variationsofsolar energy attheEarth'ssurface. 2True altitude is lower than 31,000 feet. 2changes inairpressure over the Earth's surface. 3Pressure altitude is lower than true altitude. 3movement of eirmssses from moist areas to dry areas. 6237. Which pressureis defined as station pressure? 02211. A ground basedinversionischaracterizedby 1Altimeter setting. 1convection currents at the surface. 2cold temperatures. 2Actual pressure at field elevation. 3poor visibility. 3Station barometricpressure reduced to sealevel. 6236. Isobars on a surface weather chart represent lines of 6229. What featureisassociatedwitha temperature equal pressure inversion? 1A stable layer of air. 1at the surface. 2reduced to sea level. 2An unstable layer of air. 3Airmsss thunderstorms. 3at a given atmospheric pressure altitude. 6239. En route at FL250, the altimeter is set correctly. On 6230. When does minimum temperature normally occur descent, a pilot falls to set the local altimeter setting of during a 24-hour period? 30.32. If the field elevation is 800 feet, and the altimeter is '1After sunrise functioning properly, what willItindicate upon landing? 2About 1 hcr..0 before sunrise. 9At midnight 1-1,200 feet 2-400 feet. 3Sea level.

83 f;:93 6240. En route at FL270, the altimeter is set correctly. On 6248. Which area or areas of the Northern Hemisphere descent, a pilot fails to set the local altimeter setting of experience a generally east to west movement of weather 30.57. If the field elevation is 650 feet, and the altimeter is systems? functioning properly, what willitindicate upon landing? 1Arctic only. 1-535 feet. 2Arctic and subtropical. 2-1,300 feet. 3Subtropical only. 3Sea level. 6249. At lower levels of the atmosphere, friction causes the 6241. What is corrected altitude (approximate true altitude)? wind to flow across isobars into a low because the friction 1Pressure altitude corrected for instrument error. 1decreases windspeed and Coriolis force. 2Indicated altitude corrected for temperature variation 2decreases pressure gradient force. from standard. 3creates air turbulence and raises atmospheric pressure. 3Density altitude corrected for temperature variation from standard. 6250. Which type wind flows down-slope becoming warmer and dryer? 6242. An elongated area of low pressure is called a 1Land breeze. 1trough. 2Valley wind. 2ridge. 3Katabatic wind. 3hurricane or typhoon. 6251. What is a feature of air movement in a high pressure 6243. What is an important characteristic of wind shear? area? 1it Isprimarilyassociatedwiththelateralvortices 1Ascending from the surface high to lower pressure at generated by thunderstorms. higher altitudes. 2It usually exists only in the vicinity of thunderstorms, but 2Descending to the surface and then outward. may be found near a strong temperatila 3Moving outward from the high at high altitudes and into 3It may be associated with either a wind shift or a the high at the surface. windspeed gradient at any level in the atmosphere. 6252. What is the normal direction of a valley wind? 6244. "SOUTH BOUNDARY WIND ONE SIX ZERO AT TWO FIVE, WEST BOUNDARY V IND TWO FOUR ZERO 1Up the mountain slope in the day time. AT THREE FIVE." 2Down the mountain slope in the day time. 3Up the mountain slope on the west side due to prevailing This information from the control tower indicates that westerly winds. 1a downburst is located at the center of the airport. 6253. Where is the usual location of a thermal low? 2wake turbulence exists on the west side of the active runway. 1Over the arctic region. 3there is a possibility of wind shear over or near the 2Over the eye of a hurricane. airport. 3Over the surface of a dry, sunny region.

6245. At which location does Coriolis force have the least 6254. Freezing rain encountered during climb is normally effect on wind direction? ovidence that 1At the poles. 1a climb can be made to a higher altitude without 2Middle latitudes (30' to 60'). encountering more than light icing. 3At the Equator. 2there exists a layer of warmer air above. 3ice pellets st higher altitudes have changed to rain in the 6246. How does Coriolis force affect wind direction in the warmer air below. Southern Hemisphere? 6255. What temperature condition is indicated if precipita- 1Causes clockwise rotation around a low. tioninthe tormof wet snow occurs duringflight? 2Causes wind to flow out of a low toward a high. 3Has exactly the same effect asintheNorthern 1The temperature is above freezing at flight altitude. Hemisphere. 2The temperature is above freezing at higher altitudes. 3There is an Inversion with colder air below. 6247. Which weather conditionis defined as an anti- cyclone? 1Calm. 2High pressure area. 3COL

94 84 6256. Which conditions result in the formation of frost? 6264. What is indicated about an airmass if the temperature remains unchanged or decreases slightly as altitudeis 1The temperature of the collecting surface Is at or below Increased? freezing and small droplets of moisture are falling. 2Dew collects on the surface and then freezes because 1The air is unstable. the surface temperature is lower than the air tempera- 2A temperature inversion exists. ture. 3The air is stable. 3Temperature of the collecting surface is below the dewpolnt and the dewpoint isalso below freezing. 6266. What wmther condition occurs at the altitude where the dewpoint lapse rate and the dry adiabatic lapse rate 6257. Ice pellets encountered during flight always indicate converge? that there 1Cloud bases form. 1are thunderstorms at higher levels. 2Precipitation starts. 2Is freezing rain at higher levels. 3Stable air changes to unstable air. 3is snow at higher levels. 6266. Which process causes adiabatic cooling? 6256. When will frost most likely form on aircraft surfaces? 1Expansion of air as it rises. 1On clearnightswithstableair andlightwinds. 2Movement of air over a colder surface. 2On overcast nights with freezing drizzle precipitation. 3Release of latent heat during the vaporization process. 3On clear nights with convective action and a small temperature/dm/point spread. 6267. When saturated air moves downhill its temperature increases 6256. What Is the result when water vapor changes to the liquid state while being lifted in a thunderstorm? 1at a faster rate than dry air because of tie release of latent heat. 1Latent heat is released to the atmosphere. 2at a slower rate than dry air because vaporization uses 2Latent heat is transformed into pure energy. heat. 3 Latent heat is absorbed from the surrounding air by the 3at a slower rate than dry air because condensation water droplet releases heat.

6260. What Is a feature of supercooled water? 626S. Which condition is present when a local parcel of air Is stable? 1The water drop sublimates to an ice particle upon impact 1The parcel of air resists convection. 2The unstable water drop freezes upon striking an 2The parcel of air cannot be forced uphill. exposed object 3As the parcel of air move* upward, its temperature 3The temperature of the water drop remains at 0 C until becomes warmer than the surrounding air. itimpacts a pertof the airframe, then clear ice accumulate& 6269. Convective clouds which penetrate a stratus layer can produce which threat to instrument flight? 6261. What minimum thickness of cloud layer is Indicated if precipitationisreported aslightor greaterIntensity? 1Freezing rain. 2Clear air turbulence. 1-4,000 feet thick. 3Embedded thunderstorms. 2-2,000 feet thick. 3A thickness which allows the cloud tops to be higher 6270. Which type clouds are indicative of very strong than the freezing level. turbulence?

6262. Which condition produces weather on the lee side of 1Nimbostratus. a large lake? 2Standing lenticular. 3--Ciffocumulue. 1Warm air flowing over a colder lake may produce fog. 2Cold air flowing over a warmer lake may produce 6271. What is a feature of a stationary front? advection fog. -nu warm front surface moves about half the speed of 3Warm air flowing over a cool lake may produce rain the cold front surface. showers. 2Weather conditions are a combination of strong cold 626$. Stability of the atmosphere can be determined by front and strong warm front weather. measurement of the 3 Surface winds tend to flow parallel to the frontal zone. 1 ambient temperature lapse rate. 6272. Which event usually occurs after an aircraft passes 2atmospheric pressure at various levels. through a front Into the colder air? 9surface temperature/dewpoInt spread. 1Tenveraturo/dewpoint spread decreases. 2Wind direction shifts to the left. 3Atmospheric pressure Increases.

85 95 6273. What type weather change is to be expected inan 6281. What action is recommended when encountering area where frontolysis is reported? turbulence due to a wind shift associated with a sharp 1The frontal weather is be.:oming stronger. pressure trough? 2The front is ciissipating. 1Establish a course across the trough. 3The front is moving at a raster speed. 2Climb or descend to a smoother level. 3Increase speed to get out of the trough as soon as 6274. Which weather condition isan exampleof a possible. nonfrontal instability band? 1Squall tine. 6282. Incomparisonto an approachina moderate 2Advective fog. headwind, which is an indication of a possible wind shear 3Frontogenesis. due to a decreasing headwind when descending on the glide slope? 6276. Which atmospheric factor causes rapid mowrnent of 1Less power is required. surface fronts? 2Higher pitch attitude is requireu. 1Upper winds baing across the front 3 1.ower descent rate is required. 2Upper low locateddirectly over thesurfacelow. 3The cold front overtaking and lifting thewarm front 6283. Which factor changes to cause a loss of lift when the airplane encounters a downburst during an otherwise stable 6276. Frontal waves and low pressureareas may form on ILS approach? 1warm fronts or occluded fronts 1Pitch attitude decreases. 2slow moving cold fronts or stationary fronts. 2Downward loadingofthetallsurfacesIncreases. 3cold front occlusions. 3Angle of attack decreases.

6277. What weather difference is found on each side ofa 6284. Which maximum speed Increase is recommended "dry line"? when making an approach where wind shear is suspected?

1Extreme temperature difference. 1Vu, plus 20. 2--Dewpoint difference. 2Vair plus 30. 3Stratus versus cumulus clouds. 3V, plus 30.

6278. Under what conditions would clear air turbulence 6285. What condition is necessary for the formatioi, of (CAT) most likely be ercountered? structural icing in flight? 1When constant pressure charts show 20-knot isotachs 1Supercooled water drops. less than °V NM apart. 2Water vapor. 2When constant pressure charts show 60 .knot isotachs 3Visible water. less than 20 NM apart. 3When a sharp trough is moving ata speed less than 6286. How will the airspeed Indicator react if the ram air 20 knots. Input to the pitot head is blocked by ice, but the drain hole and static port are not? 6279. Which is a necessary condition for the occurrence of 1 Indication will drop to zero. a low-level temperature Inversion wind shear? 2Indication will rise to the top of the scale. 1The temperature differential between the cold andwarm 3Indication will remain constant but will Increase in a layers must be at least 10 C. climb. 2A calm or light wind near the surface anda relatively strong wind Just above the Inversion. 6287. Whichtypeprecipitationisanindicationthat supercooled water is present? 3A wind direction difference of at least 30' betweenthe wind near the surface and the wind just abovethe 1Wet snow. inversion. 2Freezing rain. 3Ice pellets. 8280. What is the lowest cloud in the stationarygroup associated with a mountain wave? 6288. Which type of Icing is associated with the smallest 1Rotor cloud. sizo of water droplet similar to that found in low level stratus cicuds? g 2Standing lenticular. 3Low stratus. 1Clear ice. 2Frost ice. 3Rime ice.

9 86 NNW Which weather phenomenon signals the beginning of 6296. Atmospheric pressure changes due to a thunder- the mature stage of a thunderstorm? storm will be at the lowest value 1The appearance of an anvil top. 1during the downdraft and heavy rain showers. 2The start of rain at the surface. 2when the thunderstorm is approaching. 3Growth rats of the cloud is at Its maximum. 3immediately aftertherainshowers have stopped.

62110. During the We cycle of a thunderstorm, which stage 6299. Downdrafts in a mature thunderstorm are hazardous is characterized predominately by downdrafts? because they 1Cumulus. 1are kept cool by cold rain which tends to accelerate the 2Dissipating. downward velocity. 3Mature. 2converge toward a central location under the storm after striking the surface. 6291. What feature is normally associated with the cumulus 3become warmer than the surrounding air and reverse stage of a thunderstorm? into an updraft before reaching the surface.

1Beginning of rain at the surface. 6300. What is a difference between an airmass thunder- 2Frequent lightning. storm and a steady-state thunderstorm? 3Continuous updraft 1Aimuss thunderstorms produce precipitation which falls UN. What is indicated by the term embedded thunder- outside of the upd aft storms? 2Airmass thunderstormdowndraftsandprecipitation 1Severe thunderstorms are embedded in a squall line. retard and reverse the updrafts. 3Steady-state thunderstorms are associated with local 2Thunderstorms are predicted to develop in a stable airman. surface heating. 3Thunderstorms are obscured by other types of clouds. 6301. Which type storms are most likely to produce funnel clouds or tornadoes? 6293. Where do squall lines most often develop? 1in an occluded front 1Aimuss thunderstorms. 2Ahead of a cold front 2Cold trent or squall line thunderstorm. 3Storms associated with icing and supercooled water. 3Behind a stationary front.

6264. Where can the maximum hazard zone caused by 6302. When advection fog has developed, what may tend liftthe fog into low stratus clouds? wind shear associated with a thunderstorm be found? todissipateor 1In front of the thunderstorm cell (anvil side) and on the 1Temperature inversion. 2Wind stronger than 15 knots. southwest side of the cell. 2Ahear, of the roll cloud or gust front and directly under 3Surface radiation. the anvil cloud 6303. Which conditions are necessary for the formation of 3On IN sides and directly under the thunderstorm cell. uPsloPe foe 6395. Which type cloud is associated with violent turbu- 1Moist, stableair being moved over gradually rising lence and a tendency toward the production of funnel ground by a wind. coeds? 2A clear sky, little or no wind, and 100 percent relative 1Curndonknbus mamma. humidity. 3Rain falling through stratus clouds and a 10- to 25-knot 2Standing lenticular. 3Stratocumulus. wind moving the precipitation up the slope.

6296. A :leer area in a line of thunderstorm echos on a 6304. Haze layers are cleared or dispersed by radar scope indicates 1convective mixing in cool night air. 2a wind or the movement of air. 1the absence of clouds In the area. 3evaporation similar to the clearing of fog. 2an area of no convective turbdence. 3an area where predpltatlon drops are not detected. 6305. Which feature is associated with the tropopause? 6297. When flying over the top of a severe thunderstorm, 1Absence of wind and turbulence. the cloud should be overflown by at least 2Absolute upper limit of cloud formation. 3Abrupt change of temperature lapse rate. 1-1,op0 feet for each 10 knots windspeed. 2-2,500 feet 3-500 feet above any moderate to severe turbulence layer.

9 7 87r 6306. Turbulence encountered above 15,000 feet AGL, not 6314. Where is the normal location of the jetstream relative assoelated with cloud formations, should be reported as to surface lows and fronts? 1convective turbulence. 1The jetstream is located north of the surface systems. 2high altitude turbulence. 2The jetstream is located south of the low and warn 3dear air turbulence. front. 3The jetstream is located over the low and crosses both 6307. A strong wind shear can be expected the warm front and the cold front 1on the low-pressure side of a 100-knot jetstream core. 6315. Which type frontal system is normally crossed by the 2where the 20-knot isotachs are spaced 100 NM or jetstream? closer together. 3if the 5' C isotherms are spaced 100 NM or closer 1Cold front and warm front together. 2Warm front 3Occluded front 6308. A most likely location of clear air turbulence is 6316. Which type clouds may be associated with the 1in an upper trough on the polar side of a jetstream. 2near a ridge aloft on the equatorial side of a high jetstream? pressure flow. 1Cumulonimbus cloud line where the jetstream crosses 3downstream of the equatorial side of a jetstream. the cold front 2Cirrus clouds on the equatorial side of the jetstream. 6309. The strength and location of a jetstream is normally 3Cirrostratus cloud band on the polar side and under the 1stronger and farther north in the winter. jetstream. 2weaker and farther north in the summer. 6317. Which action is recommended if jetstream turbulence 3weaker and farther south in the winter. is encountered with a direct headwind or tailwind? 6310. Where do the maximum winds associated with the 1Increase airspeed to get out of the area quickly. jetstream usually occur? 2Change course to fly on the polar side of the jetstream. 1In the vidn11 , of breaks in the tropopause on the polar 3Change altitude or course to avoid a possible elongated side of the jet core. turbulent area. 2Below the jet core where a long straight stretch of the jetstream is located. 6318. Which action is recommended regarding an altitude 3On the equatorial side of the jetstream where moisture change to get out of jetstream turbulence? has formed drriform clouds. 1Descend if ambient temperature is falling. 2Descend if ambient temperature is rising. 6311. Which type jetstream can be expected to cause the 3Maintain altitude if ambient temperature is not changing. greater turbulence? 6319. Clear air turbulence associated with a mountain wave 1A straight jetstream associated with a high pressure may extend as far as . 2A jetstream associated with a wide isotherm spacing. 1-1,000 miles or more downstream of the mountain. 3A curving jetstream associated with a deep lowpressure 2-5,000 feet above the tropopause. trough. 3-100 miles or more upwind of the mountain.

6312. What weather feature occurs at altitude levels near 6320. Summer thunderstormsin the Arctic regionwill the tropopause? generally move 1Maximum winds and narrow wind shear zones. 1northeast to southwest in polar easterlies. 2Abrupt temperature increase above the tropopause. 2southwest to northeast with the jetstream flow. 3Thin layersofcirrus(icecrystal)cloudsatthe 3directly north to south with the low level polar airflow. tropopause level. 6321. Which arctic flying hazard is caused who a cloud 6313. Where are jetstreams normally located? layer of uniform thickness overlies a snow or ice covered surface? 1In areas of stronglow pressure systemsinthe stratosphere. 1Ice fog. 2At the tropopause where intensified temperature gradi- 2Whiteout. ents are located. 3Blowing snow. 3In a single continuous band, encircling the Earth, where there Is a break between the equatorial and polar tropopause.

98 88 6322. Which weather conditionis aociated with the 6331. (Refer to figure 120.) The SP report at Galveston Intertropical Convergence Zone" near the Equator? (GLS) indicates which condition?

1-Permanent low-pressure area at the surface. 1-Wind 170' magnetic at 5 knots. 2-Air rising, frequent thunderstorms, and heavy rains. 2-No precipitation since last synoptic report. 3-Development of tropical cyclones which may grow Into 3-Sea level pressure 1000.7 millibars. hurricanes or typhoons. 6332. (Refer to figure120.) What was the difference 6323. Which weather condition is present when the tropical between the reported weather at Houston Hobby (HOU) and storm is upgraded to a hurricane? Houston International (IAN)?

1-Highest windepeed, 100 knots or moi..N. 1-HOU had a higher ceiling. 2-A clear area or hurricane eye has formed. 2-Wind direction was more southerly at IAH. 3-Sustained winds of 65 knots or more. 3-IAH had better visibility.

6324. What is the general direction of movement of a 6333. (Refer to figure 120.) What weather improvement was hurricane located in the Caribbean or Gulf of Mexico region? reported at Lubbock (LBB) between 1750 and 1818 UTC? 1-Northwesterly curving to northeasterly. 1-The rain showers stopped. 2-Westerly, until encountering land, then easterly. 2-The ceiling improved by 1,800 feet. 3-Counterclockwise over open water, thendissipating 3-Visibility improved. outward over land. 6334. (Refer tofigure120.) What cloud conditionis 6325. (Refer to figure 120.) What was the local Central indicated by a B-727 pilot over Lubbock (LBB)? Standard Time of the surface report at Austin (AUS)? 1-- Ceiling was at 4,500 teat MSL 1-11:53 a.m. 2-Base of broken clouds was at 4,500 feet AGL 2-5:53 p.m. 3-Cloud tops varied between 5,300 feet and 6,000 feet 3-10:53 p.m. MSL

6326. (Refer to figure 120.) What type of report is listed for 6335. (Refer to figure 120.) What weather condition is DelhaR (DHT)? indicated by the report at Midland (MAF)? 1-A report made by an automatic weather reporting 1-Rain of unknown intensity was observed in the 090 to system. 180 quadrant 2-A special report concerning very low station pressure. 2-The ceiling was at 25,000 feet MSL 3-A record of a special report about a significant weather 3-Wind was 020' magnetic at 20 knots. change. 6336. (Refer to figure 121.) What information is contained 6327. (Refer to figure 120.) Wit method was used to in the PIREP at San Antonio (SAT)? obtain the SP report at Marfa (MRF)? 1-lime of report was unknown. 1-Staffed AMOS station. 2-Type of aircraft was unknown. 2-Automatic weather observing station (AMOS). 3-Top ofthe scatteredlayer was 4,000 feet AGL 3-A military station observation of temperature, dewpoint, wind, and station pressure only. 6337. (Refer to figure 121.) What change took place at WichitaFalls(SPS) between1757and 1820 UTC? 6326. (Refer to figure 120.) What condition is reported at Childress (CDS)? 1-The rain became heavier. 2-Atmospheric pressure increased. 1-Distant heavy rain showers. 3-The ceiling lowered. 2-Heavy rain showers began 20 minutes after the hour. 3-The ceiling is solid overcast at an estimated 1,800 feet 6336. (Refer to figure 121.) What was the ceiling at Fort above sea level. Smith (FSM)?

6329. (Refer to figure 120.) What condition is reported at 1-8,000 feet AGL. Dallas (DAL)? 2-2,500 feet AGL. 3-2,900 feet MSL 1-The station pressure Is 1008.7 millibars. 2-Temperature/dewpoint spread is 16' C. 6339. (Refer to figure 121.) What change had taken place 3-Altimeter setting is 30.07. between 1755 and 1825 UTC at Harrison (HRO)?

6330. (Refer to figure 120.) The pilot report at Fort Worth 1-Wind shifted from south to north-northwest. (FTW) indicates 2-Thundershowers began at 25 minutes after the hour. 3-Visibility reduced to IFR conditions. 1-several overcast layers including one above 9,500 feet. 2-a clearlayer between 3,600 feetand 6,000 feet. 3-the base of an overcast layer at 7,500 feet

89 99 6340. Runway visual range is measured in which of the 6348. Weather satellite images show tropopause weather foNowing units? by reporting which reflections from the surface and clouds? 1Maters/1,000. 1Ultraviolet and infrared reflections. 2Feet/100. 2Infrared and visible light reflections. 3Milse and fractions of miles. 3Solar radiation and terrestrial radiation.

6341. The purpose of the transmissometer is to measure 6349. What Is the single source reference that contains 1braidng action on a wet runway. information regarding frontal movement, turbulence, and icing conditions for a specific region? 2the bases of obscuring precipitation. 3the distance apilot can see down the runway. 1Weather Depiction Chart. 2Area Forecast 6342. Which measurement is reported as runway visibility? 3Terminal Forecast 1Visibility reported by a ground observer from the airport control tower. 6350. Which primary source contains Information regarding 2Slant range visibility in the landing area of the active the expected weather at the destination airport and at the ETA? runway. 3Distance down the runway a pilot can see unlighted 1Low Level Prog Chart. objects. 2Radar Summary and Weather Depiction Charts. 3Terminal Forecast 6343. What does the RVR value depicted on instrument approach procedure charts represent? 6361. The body of a Terminal Forecast covers a geographi- E. cal area within 1The horizontal distance a pilot can see high -intensity runway lights. 1a 5-mile radius of the center of a runway complex. 2The horizontal distance down the runway a pilot cansee 2-25 miles of the center of an airport unkihtlid Ant& 3-10 miles of the station originating the forecast. 3The slant visual range a pilot will see down the final approach during landing. 6362. The absence of a visibilityentry in a Terminal Forecast specificallyImpliesthat the surface visibility 6344. If squalls are reported at the destination airport, what wind conditions existed at the time? 1is at least 1 SM above the minimum visibility requirement for an approach to the primly instrument runway. 1Sudden increases in windspeed of at least 15 knots, 2exceeds 6 SM. lasting for at least 1 minute. 3Is at least 15 SM in all direntions from the center of the 2--Peak gusts of at least 35 knots for a sustained period of runway complex. 1 minute or longer. 3Rapid variation in wind direction of at least 20' and 6353. What sources reflect the most accurate information changes in speed of at least 10 knots between peaks on current and forecast icing conditions? and kills. 1Low Level Sig Weather Prog Chart, RADAT's, and the 63411. Which type of weather can only be directly observed Area Forecast. during flight and then reported in a PIREP? 2PIREP's, Area Forecast, and the Freezing Level Chart. 3PIREP's, AIRMET's, and SIGMET's. 1--Structural icing. 2Jetstream type winds. 6354. What weather Ispredicted by the term "TRW 3Level of the tropopause. VICINITY" in a Terminal Forecast?

6346. What Is indicated by a PIREP which is preceded in 1Thunderstorms are expected between 5 and 25 miles of the Surface Weather Report by theletters"UU/t"? the runway complex. 2Rain showers may occur over the station and within 1Unconfirmed PIREP. 50 miles of the station. 2Urgent PIREP. 3Scattered thundershowers arepredicted within the 3PIREP from an unknown type aircraft and at an unknown Terminal Control Area. flight altitude. 6355. (Refer to figure 122.) What weather is predicted at 6347. Which pattern on a weather radar scope Isan Alice TX (ALI) at 15002? indication of a tornado? 1Marginal VFR due to ceilings. 1A hook echo. 2Surface wind gusting to 25 knots. 2A line echo wave pattern. 3Visibility 8 statute miles In haze. 3An echo indicating severe hail.

90 one 6366. (Refer to figure 122.) The categorical outlook for 6365. TWEB Route Forecasts provide predicted weather for Austin (AUS) indicates 1-a corridor 25 miles either side of a numbered cross- 1-marginal VFR due toceilingsand thunderstorms. country route. 2-a chance of 1,000 feet AGL cab cgs. 2-a 50-mile radius of the takeoff and landing airports. 3-ailing 1,400 broken and thunder showers. 3-any route of flight specified by the requesting pilot

6357. (Refer to figure 122.) At which time is IFR weather 6366. How can the pilot obtain TWEB Route Forecast first predicted at Lubbock (LBB)? information? 1 1-1500Z. 1-From the TEL TWEB and Telephone Voice Response 2-1700Z. Systems (VRS). 3-0900Z. 2-From the ATIS and Pilots Automatic Telephone Weather. 3-From ARTCC and Automated Flight Service Station 6358. (Refer to figure 122.) What type conditions can be briefings. expected for a flight scheduled to land at San Angelo (SJT) at 1500Z? 6367. What information is provided by this TWEB Route Forecast excerpt? 1-Chance of 1 nautical mile visibility. 2-Occasional ceilings 800 feet in thunderstorms. 249 TWEB 252317 GFK-M01-ISN, GFK VCNTY CIGS AOA 3-IFR conditions due to low ceilings,rain, and fog. 5 THSD TILL 12Z...

6359. (Refer to figure 123) The weather system forecast 1-Grand Forks (GFK) ceilings at or above 5,000 feet MSL from Tennessee to Texas is expected to be influenced by a 2-Route No. 249, from GFK to MO1 to ISN. 3-Ceilings within a 50-mile radius of Grand Forks (GFK) 1-dry line producing thunderstorms. are 5,000 feet AGL 2-warm front in the east and cold front in the west. 3-stationary front with moist, low-level flow. 6388. (Refer to figure 124.) Which system in the Convective Sigmet listing has the potential of producing the most 6360. (Refer to figure 123.) The area forecast indicates that severe storm? aviation weather hazards are predicted for 1-The storms in Texas and Oklahoma. 1-OK, AR, TN, AL, and DC. 2-The stormsinColorado,Kansas, and Oklahoma 2-TX, LA, MS, AR, and Coastal Waters. 3-The isolated storm 50 miles northeast of Memphis 3-0K, AR, LA, TN, MS, AL, TX, and Coastal Waters. (MEM).

6361. (Refer to figure 123.) According to the forecast, the 6369. (Refer to figure 124.) What time period is covered by freezing level is expected to be the outlook section of the Convective Sigmet? 1-18,000 feet MSL with icing in south Texas. 1-24 hours after the valid time. 2-13,000 feet MSL in northern Arkansas and Tennessee. 2-2 to 6 hours after the valid time. 3-13.000 feet AGL in northern Oklahoma. 3-No more than 2 hours after the valid time.

6362. (Refer to figure 123.) The forecast for IFR conditions 6370. Which type weather conditions are covered in the in Texas and Oklahoma anticipates Convective Sigmet? 1-ceilings of 1,000 feet MSL or less. 1-Embedded thunderstorms, lines of thunderstorm, and 2-visibility restrictions due to fog. thunderstorms with 3/4 inch hail or tornadoes. 3-turbulence in the stratus layers to as high as 24,000 feet 2-Cumulonimbus clouds with tops above the tropopause MSL and thunderstorms with 1/2 inch hail or funnel clouds. 3-Any thunderstorm with a severity level of VIP 2 or more. 6363. (Refer to figure 123.) What is the categorical outlook for the areas of Texas and Oklahoma where thunderstorms 6371. (Refertofigure125.) What approximate wind are predicted? direction, speed, and temperature (relative to ISA) are 1-Light rain and scattered, embedded thundershowers. expected for a flight over OKC at FL370? 2-Cumulonimbus clouds with tops up to 35,000 feet MSL 1 -265' true; 27 knots; ISA + 1' C. 3-Callings lowering from 1,500-2,500 feet AGL to less than 2-2806 true; 27 knots; ISA +6' C. 1,000 feet AGL 3-260' magnetic; 27 knots; ISA -5' C.

NU. (Refer to figure 123.) What weather is forecast for 6372. (Refertofigure125.)What approximate wind extreme Western Tennessee? direction, speed, and temperature (relative to ISA) are expected for a flight over TUS at FL270? 1-Mountains obscured by low stratus clouds and precipitation. 1-347' magnetic; 5 knots; ISA -10' C. 2-Generally ceilings 9,000 feet AGL, occasional ceilings 2-350' true; 5 knots; ISA +5' C. 1,500-2,500 feet AGL 3-0106 true; 5 knots; ISA +136 C. 3-IFR ceilings due to thunderstorms. 11373. (Refer to figure125.) What approximate wind 6382. What wind direction and speed aloft are forecast by direction, speed, and temperature (relativeto ISA) are this FD report for FL390- "750649"? expected for a flight over INK at 16,000 feet? 1-350' at 64 knots. 1-025' magnetic; 7 knots; ISA -10' C. 2 -250' at 106 knots. 2-035' true; 8 knots; ISA +5' C. 3-150' at 6 knots. 3-030' true; 7 knots; ISA +15' C. 6303. What wind direction and speed aloft are forecast by 6374. (Refer tofigure125.) What approximate wind this FD report for FL390- "731960"? direction, speed, and temperature (relativeto ISA) are expected for a flight over JAN at FL350? 1-230' at 119 knots. 2-131' at 96 knots. 1-230' true; 2 knots; ISA +10' C. 3-073' at 196 knots. 2-295' true; 8 knots; ISA -10' C. 3-230' magnetic; 3 knots; ISA +5' C. 6384. (Refer to figure 126.) Which marginal VFR condition was reported in north-central Wyoming? UM (Refer tofigure125.)What approximate wind direction, speed, and temperature (relative to ISA)are 1-Sky obscured, visibility restricted by smoke. expected for a flight over MKC at FL260? 2-Sky partiallyobscured,ceiling2,000 feet,visibility 5 miles in haze. 1-260' true; 43 knots; ISA +10' C. 3-Broken ceiling measured at 200 feet 2-280' true; 45 knots; ISA -10' C. 3-280' magnetic; 42 knots; ISA +9' C. 6385. (Refer to figures 126 and 127.) Which conditions caused the IFR weather which was reported in West 6378. (Refer to figure 125.) What will be the windand Virginia? temperature trend for a HOU-DAL-OKC flight at FL390? 1-Heavy thundershowers. 1-Wind direction shift from north to west. 2-Visibility 2-4 miles in rain. 2-Windspeed increase. 3-Sky obscured, visibility less than 1 mile in fog. 3-Temperature decrease. 6386. (Refer to figures 126 and 127.) The IF:, conditions 6377. (Refer to figure 125.) What will be thewind and behind the cold front in central Georgia were mostly a result temperature Vend ft a SAT-ELPTUS flight at 16,000feet? of

1-Temperature decrease slightly. 1-continuous rain and low ceilings. 2-VVindspeed decrease. 2-thunderstorms with tops over 30,000 feet. 3-Wind direction shift from southeast to east. 3-warm, moist air flowing inland from Atlantic coastal waters. 8378. (Refer to figure 125.) What will bethe wind and temperature trend for a STL-MEM-MSY flightat FL330? 8387. (Refer to figures 126 and 127.) The thunderstorm 1-Windspeed decrease. area in northern Georgia was moving 2 -Wind shift from west to north. 1-the same direction as the cold front. 3-Temperature Increase 5' C. 2-north-northeast at 20 knots. 3-southeast with tops of 21,000 feet. 4379. (Refer to figure 125.) What will bethe wind and temperature trend for a DEN-ICT-OKC flight at11,000 feet? 6388. (Refer to figures 126 and 127.) A flight from New 1-Temperature decrease. Orleans to central Florida over the Gulf from 10002 to 2- Windepeed increase slightly. 1135Z would probably have encountered 3-Wind shift from calm to a westerly direction. 1-IFR conditions with continuous rain, conditions improving after passing the cold front. 6380. (Refer to figure 125.) What will bethe wind and 2-strong to very strong temperature trend for a DSM-LIT-SHV flic;it at 12,000 thunderstorms with tops of feet? 30,000 feet or higher. 1-Windspeed decrease. 3-marginal VFR conditions with thundershower intensity 2-Temperature decrease. decreasing. 3-Wind directionshiftfrom northwest tosoutheast. 6389. (Refer to figure 127.) The thunderstorm area ap- 6381. (Refer to figure 125.) What is the forecasttempera- proaching the Washington, DC vicinity from Virginia was ture at ATL for the 3,000-foot level? moving 1- +6' C. 1-northeast at 30 knots. 2- +6' F. 2-north at 17 knots. 3- Not reported. 3-north-northeast at 15 knots.

92 102 6300. (Refer to figures 128 and 127.) A flight planned from 6397. A Weather Depiction Chart indicates Washington, DC to Atlanta (north-central Georgia) at 12002 should expect 1actual sky cover,visibilityrestrictions, and type of precipitation at reporting stations. 1thunderstorms with tops in the vicinity of 21,000 feet 2forecast ceilings and visibilities over a large geographic 2a wind shift because of passing through a cold front area.

3VFR or marginal VFR conditions for the entire flight. 3- -acts. I en route weather conditions between reporting stations. 8391. (Refer to figures 128 and 127.) The IFR weather off the New Jersey shore and approaching New York City In the 6398. What is indicated on the Weather Depiction Chart by warm front included a continuous smooth line enclosing a hatched geographic area? 1a strongthunderstormareamovingnortheastat 10 knots. 1The entire area has ceilings less than 1,000 feet and/or 2a VIP 3 to 4 thunderstorm area with a cell top of visibility less than 3 miles. 27,000 feet. 2More than 50 percent of the area enclosed by the 3marginal VFR conditions with ceilings of 6,000 feet, smoothlineispredicted to have IFRconditions. visibility E miles in light fog. 3Reporting stations within the enclosed area are all showing IFR conditions at the time of the report 6392. (Refer to figure 127.) The thunderstorms in the Gulf to the south of the western Florida panhandle contained 6399. For the most effective use of the Radar Summary Chart a flight planner should 1a very strong storm area with all tops above 40,000 feet. 2thunderstormswithlittlemovement andtopsof 1consult the chart to obtain the most accurate measure- 18,000 feet ment of freezing levels, cloud cover, and wind conditions 3at least one strong to very strong cell with a top above between reporting stations. the tropopsuse. 2compare the chart information with the Weather Depic- tion Chart to get a three-dimensional picture of clouds 6393. (Refer to figure 128.) The cold front stretching from and precipitation. the Great Lakes to the Texas Panhandle is drawn to show 3analyze the chart for information on ceilings, cloud tops, its position and cloud coverage between reporting stations. 1-8 hours after the chart was issued. 6400. What information is provided by the Radar Summary 2-1 hour before the reported IFR and MVFR contour line Chart thatisnot shown onother weather charts? posilions 3-1 hour before the forecast weather at each reporting 1Lines and .ells of hazardous thunderstorms. station. 2Types of precipitation between reporting stations. 3 Ceilings and precipitation between reporting atations. 6394. (Refer to figures 128 and 127.) Which conditions were reported by those stations in Arizona which did not 6401. (Refer to figure 128.) Which conditions are predicted report clear skies? for southern Florida on the 24-Hour Surface Prognostic Chart? 1 Breaks In the overcast 2Scattered to broken clouds. 1Moderate to severe turbulence over more than half the 3Radar observations unavailable. area. 2Rain showers and thunderstorms over less than half the 6396. (Refer to figures 128 and 127.) The IFR conditions in area. the vicinity of Lakes Superior, Huron, and Michigan were 3MVFR flight conditions. caused by 6402. (Refer to figure128.) Th3 warm front along the 1overcast sky and haze. southeast states coastal areas will be producing 2convective action during the cold front passage. 3obscured skies and fog. 1showery precipitation covering half or more of the area. 2continuous IFR conditions with rain and thundershowers. 6396. What is a feature of the Radar Summary Chart? 3high winds due to hurricane Florence.

1 Severe weather watches are shown for the valid time. 6403. (Refer to figure 128.) What type weather will be 2Tops and bases of all cloud cover in the reporting area associated with the cold front depicted from Canada through are shown. the south-central states? 3Predicted locationofsolidthunderstormlinesare highlighted. 1Convective activity in Texas and Oklahoma. 2Moderate turbulence and scattered rain showers in the Great Lakes area. 3Continuous rain and rain showersinsouth-central Cans 103 93 ,

:;..%+., 6404. (Refer to figure128.) What type turbulence is 6412. The effectiveness of applied Freezing PointDepres- expected in the southeastern state area? sant (FPD) fluid during snow or freezing precipitation will 1-Light to moderate turbulence up to the 240 millibar levsl. 1-remain at full strength until takeoff. 2-Severe clear air turbulence up to FL240. 2-deteriorate as water is absorbed inthe FPD film. 3-Moderate to severe turbulence from thesurface to 3-become better as hot air type anti-ice systems 24,000 feet MSL. are activated during the taxi-out period. 6406. (Refer to figure 128.) The freezing level in the Like 6413. Which source is recommended foran initial look at Michigan area is forecast to be the weather expected for a planned flight? 1-above the turbulence level. 1-En Route Flight Advisory Service (EFAS). 2-at the surface. 2-Hazardous In-Flight Weather Advisory Service (HIWAS) 3-at the 120 millibar level. 3-A.M. Weather Telecast on PBS. 6406. (Refer to figure 128.) What type weather is associ- 6414. What method can be used to get recorded weather ated with the low-pressure areas in California? information from theInterimVoice Response System 1-Moderate turbulence up to 12,000 feet MSL (IVRS)? 2-Low ceilings due tothe approaching coldfront 1-Contact the AFSS on a localor long distance telephone 3-Unusually low barometric pressure. line for a personal briefing. 6407. (Refer to figure 128.) What is the 2-Use a touch-tone telephone and follow recordedmenu forecast activity of instructions. the trough in eastern Montana during the0000Z to 1200Z perbd? 3-Contact the local FSS using a rotary dialtelephone and follow recorded instructions. 1-Completely dissipate due to the strengtheninghigh- pressure area. 6415. What basic information is providedautomatically by 2-Move southward and merge with thewestern half of the the Interim Voice Response System (IVRS)recording? cold front 1-Surface Observations, Terminal Forecasts, WindsAloft 3-Move eastward into the Lake Superiorarea. Forecasts, and Selected Weather Warnings. 6406. (Refer to figure 128.) Which location 2-Terminal Forecasts, Radar Summaries, Weather Depic- includes a tion, and AIRMET's. prediction of continuous rain? 3-Observed weather at the takeoff and landing airports, 1-Central Gulf of Mexico. and current ATIS recordings. 2-South-central Canada. 3-Coastal areas of Georgia and the Carolinas. 6416. What information does the pilot supply to obtain recorded weather related to the flight from the Interim Voice 6401. (Refer to figure 128.) Whatweather information is Response System (IVRS)? shown for the storm system whichhas been named "Florence"? 1-Telephone number where the FSS briefercan contact the pilot. 1-The system is a tropical cyclone withno associated 2-Location identifiers (LOCIDS), route, altitude, and times thunderstorms. for the flight 2-The system will develop'.J hurricane strength between 3-Flight information in the same order ason the FAA Flight 0000Z and 1200Z Sep 09. Plan Form. 3-The storm is moving toward andmerging with the warm front. 6417. An unscheduled air traffic advisory, for use by air carrier crews to anticipate and avoid adverse weather ata 6410. (Refer to figure 128.) Whatare the lowest and busy terminal is known as highest sea level atmosphericpressures predicted on the 24-Hour Surface Prog Chart? 1-center weather advisories (CWA). 2-severe weather watch bulletins (WW). 1-1008.0 millibars to 1018.0 millibars. 3-special flight forecasts (SFF). 2-1000.0 millibars to 1018.0 millibars. 3-1004.0 millibars to 1011.8 millibars. 6418. Which forecast provides specific informationconcern- ing expected sky cover, cloud tops, visibility, weather, and 8411. Freezing Point Depressant (FPD) fluidis intended to obstruction to vision in a route format? be applied 1-DFW FA 131240. 1-es an anti -ice and deice mediumbeforetakeoff. 2-249 TWEB 252317. 2-during flight, to wings and critical surfacesnot protected 3-CHI WA 300300. by a hot air anti-ice system. 3-on the ground during snowor freezing rain to all air carrier airplanes and helicopters.

- 10A 6419. Forecast winds and temperaturesaloftfor an 8427. Below FL180, en route weather advisories should be IMernational flight may be obtained by consulting obtained from an FSS on 1-Area Forecasts published by the departure location host 1-122.1 MHz. country. 2-122.0 MHz. 2-the current International Weather Depiction Chart appro- 3-123.6 MHz. priate to the route. 3-Wind and Temperature Aloft Charts prepared by a 8428. What type turbulence should be reported when it Regional Area Forecast Center (RAFC). causes slight, rapid, and somewhat rhythmic bumpiness without appreciable changes in attitude or altitude, less than 6420. How will an area of thunderstorm activity, that may one-third of the time? wow to severe intensity, be Indicated on the Severe Weather Outlook Chart? 1-Occasional light chop. 2-Moderate turbulence. 1--SLGT within canoes - hatched areas. 3-Moderate chop. 2--APCHG within any area 3-SVR within any area 6429. What type turbulence should be reported when it causes changes in altitude and/or attitude more than two- 11421. For internationalflights, a High Level Significant thirds of the time, with the aircraft remaining In positive Prognostic Chart is prepared for use at control at all times?

1 -any flight level above 290. 1- Continuous severe chop. 2--F1.250 to FL600. 2-Continuous moderate turbulence. 3-FL180 to FLOOD. 3-Intermittent moderate turbulence.

0422. The Low Level Prognostic Chart depicts weather 6430. What type turbulence should be reported when it conditions momentarily causes slight erratic changes in altitude and/or attitude, one-third to two-thirds of the time? 1-that are forecast to exist at a specific time shown on the 1-Occasional light chop. 2-es they existed at the time the chart was prepared. 2-Moderate chop. 3-that are forecast to exist 6 hours after the chart was 3-Intermittent light turbulence. prepared. 6431. (Refer to figures 129 through 131.) What is the wind 11423. A station is forecasting wind and temperature aloft to velocity at 39,000 feet around the low pressure center in be MO' at 205 knots; temperature -51' C at FL390. How Canada? would this data be encoded in the FD? 1-10 knots. 1-7800-51. 2-20 knots. 2-789951. 3-30 knots. 3-280051. 6432. (Refer to figure 129.) Which area has the greatest 6424. At what time are current AIRMET's broadcast in their potential for condensation as inferred by the entirety by the AFSS? temperature/dewpoint spread on the 500 MB Constant Pressure Chart? 1-15 minutes after the hour only. 2-Ever,15 minutesuntilthe AIRMET iscanceled. 1-Along the Oregon and California coast. 3-15 and 45 minutes after the hour during the first hour 2-Western U.S. along the 55880 meter height contour. after issuance. 3-Around the low pressure center in Canada

MK If a SIGMET alert is announced, how can information 6433. (Refer to figures 129 through 131.) Which flight level contained in the SIGMET be obtained? should afford the best wind conditions for a northbound flight along the California Coast? 1-ATC willannounce the hazard and advise when Information will be providedInthe FSS broadcast 1-FL180. 2-By contacting a weather watch station. 2-FL280. 3-By contacting the nearest AFSS. 3-FL380.

6426. What type service should normally be expected from 6434. (Refer to figure 131.) What Is the height of the an En Route Flight Advisory Service? 200 MB levelat the low-pressure center in Canada?

1-Weelther advisoriespertinent tothe type offlight, 1-1,850 meters MSL Intended route of flight, and altitude. 2-18,500 meters MSL 2-Severe weather information, changes In flight plans, and 3-11,850 meters MSL mosipt of position reports. 9 -Radar vectorsfortrafficseparation,route weather advisories, and altimeter settings.

9 5 '105 6436. (W.* to figure 130.) What isthe height of the 6442. (Refer to figures 129 through 131.) What movement 300 MB levelat the low pressure center in Canada? of the LOW in Mexico is inferred by the winds plottedon the 1-9,120 meters MSL Constant Pressure Charts? 2-18,000 meters MSL 1 -Very slow movement. 3-11,850 meters MSL 2-Rapid movement 3-Northward movement. 6436. Interpret the path of the jetstreamfrom figures 129 through 131. 6443. (Refer to figure 129.) What change in height ofthe 500 MB level over central Oklahoma has occurred in 1-Southern California, Nevada, Utah,Nebraska/Kansas, the and then southeastward. last 12 hours? 2-Oregon, Idaho, Wyoming, Nebraska, Iowa,and across 1-Lowered 300 meters. the Great Lakes. 2-Raised 30 meters. 3-The Alaska area, across Canada toMontana, North 3-Raised 20 meters. Dakota, then across the Great Lakesarea 6444. From figures 132A through 132D, determinean area 6437. The systemdepictedon the 500 MB chart, of potential wind shear. F- figure 129, that is approaching the California Coastfrom the west is a 1-South central Canada. 1-LOW. 2-Northeast United States coast and Canada. 2-HIGH. 3-Over the Pacific Ocean west of the United Statescoast 3-cold front 6445. (Refer to figures 132A through 132D.) What isthe direction of windflow along the United States Atlanticcoast? 6438. What type weather is inferred by thealmost vertical extent of the LOW in Canada as depicted in figures129 1-Westedy. through 131? 2-Northeasterly. 3-Southwesterly. 1-A rapid moving system with little chanceof developing cloudiness, precipitation, and adverse flyingconditions. 6446. From figures 132A through 1320, determinethe 2-A slow moving storm which may came extensive and forecast position of the jetstream at thetropopause. persistent cloudiness, precipitation, and generallyad- verse flying weather. 1-From the California/Mexico border eastwardacross the 3-A rapid moving storm, leaning towest with altitude, southern states and cver the Atlantic Ocean east of Florida. which encourages line squalls ahead ofthe system with a potential of severe weather. 2-From central California eastwardacross the United States and northeastward across the Atlantic Ocean 6439. (Refer to figures 129 through 131.)What is the from North Carolina approximate temperature for a flight from southernCalifornia 3-From the Alaska area southeastward to Montana and to central Kansas at FL350? North Dakota, across the Great Lakes to New York and 1- -16' C. then northeast over the Atlantic. 2- -39' C. 8447. (Refer to figures 132A through 132D.) What vertical 3- -41' C. wind shear can be expected at the tropopauseon a line from the Great Lakes to Flirida? 6440. (Refer to figures 129 through 131.)Determine the approximate wind direction and velocity at FL240over the 1-60 knots. station in ovntral Oklahoma. 2-30 knots. 3-2 knots. 1-280' at 10 knots. 2-3206 at 10 knots. 6448. (Rote: to figures 132A through 132D.) What is the 3-330' at 13 knots. approxinw:te height of the tropopause over most of the United States? 6441. (Refer to figures 129 through 131.)What is the relative moisture content of the aimlessapproaching the 1-35,000 to 45,000 feet. California coast? 2-45,100 to 50,000 feet. 3-Over 50,000 feet. 1-Dry. 2-Moist enough for condensation. 6449. (Refer to figures 132A through 132D.) Whatare the 3-Yery wet with high potential for clouds andprecipitation. strongest observed winds at the tropopause? 1-70 knots. 2-80 knots. 3-90 knots.

96 106 6450. (Refer to figure 132C.) What are the coverage and 6458. An ISOGRIV is defined correctly by which of the vertical extent of the isolated embedded thunderstorms over following responses? Line of the southeastern United States? 1equal grivation. 1one-eighth to five-eighths coverage, surface to FL420. 2equal variation. 2one-eighth to five-eighths coverage, below FL240 to 3zero grivation. FL450. 3Less than one-eighth coverage, below FL240 to FL420. 8459. Which chart projection is most commonly used for grid flights in subpolar areas? 6451. (Refer to figure 132C.) The large arrow over the 1Lambert conformal. north-central, United States depicts 2-- Gnomonic. 1the jetstreamtobe 90 knotswest-eouthwestat 3Mercator. 37,000 feet. 2thunderstorm movement with winds in the thunderstorms 6460. Grid meridians often are parallel to the at 90 knots. 1Equator. 3strongest winds at the tropopause to be 90 knots from 2-180' meridian. west-southwest. 3Greenwich Meridian. 6452. (Refer to figure 132C.) What turbulence is expected 8481. Which chart projection is used only for planning grid In the Florida area as implied by the High Level Significant polar flights? Weather Chart? 1Transverse Mercator. 1Light to moderate. 2Polar stereographic. 2Moderate or greater. 3Polar gnomonic. 3Severe. 6462. Which chart projection is most commonly used for 6453. The shaded area labeled "MDT" in figdres 133A and aeronautical navigation? 1338 represents 1Mercator. 1moderate intensity thunderstorms. 2Lambert conformal. 2severe thunderstorms with a coverage of 6 to 10 per- 3--Stereographic. cent of the area. 3moderate weather with embedded thunderstorms of 6463. Which features are associated with the Lambert unknown intensity. Conformal Conic Projection? 6454. (Refer to figures 133A and 133B.) What is the 1A straight line approximates a great circle. primary purpose of the Severe Weather Outlook charts? 2Meridians are straight lines, equally spaced. 3Straight linescross meridiansat constant angles. 1Advanced planning for future storm development 2 Specific information on intensity of severe weather. 6464. Which publication deals solely with solutions con- 3 Positive information on severe weather in progress. cerning selected stars? 6456, (Refer to figures 133A and 133B.) In what areas are 1H.O. Pub. No. 249, Sight Reduction Tables, Volume I. probable general thunderstorm activity forecast? 2H.O. Pub. No. 249, Sight Reduction Tables, Volume II. 3H.O. Pub. No. 249, Sight Reduction Tables, Volume III. 1 In the shaded area labeled "LGT." 2Between the two lines with an arrowhead. 6465. How are select stars that are best suited for fixing 3On the east of each line with an arrowhead. purposes identifiedin the H.O. Pub. No.249,Sight Reduction Tables? 6456. What information is indicated by the note, "APCHG" In figure 133A? 1Name printed in bold type. 2Marked by a number symbol. 1Approaching storms are forecast to have large hail 3Marked Li diamonds. 3/4-inch in diameter. 2Approaching storms deteriorating with clearing the next 6466. Precession and nutation corrections arc only applied 12 hours. to 3Probable general thunderstorm activity may approach severe intensity. 1the Moon. 2select stars. 41467. Convergence on a grid chart is defined as the angle 3the Sun. behveen 6467. Nutation is defined as 1grid north and true north. 2magnetic north and true north. 1bending of the light as it passes through the atmos- 3grid north and magnetic north. phere. 2error caused by mechanical faultsinthe sextant. 3nodding or wobbling of the Earth on its axis. 97 107 11466. When is parallax error the greatest? 6477. HON can latitude be determined from a celestial 1-When the body being observed ison the horizon. observation of Polaris? 2-When the HS is greatest (Leg close to 90). 1-By applying a Coriolis correction to the HO (observed 3-When the attitude of the observeraircraftishigh. altitude). 2-By applying a "0" correction to the r-!0 (observed 6460. A parallaxcorrectionis applied to a celestial altitude). observation of the 3-By using the formula R ... RO X f. 1-Sun. 2-planets. 6476. A line extending southward from the western side of 3-Moon. the square of Pegasus leads to the star 1-Diphda. 0470. What causes refraction error ina sextant? 2-Fomalhaut 1-Improper alignment of the optical system in thesextant. 3- Achenar. 2-Poorly aligned sextant mount In the aircraft 6479. The firstmagnitudestar 3-Bending of the light as it passes through theatmos- approximately midway phere. between Betelgeuse and the Pleiades Is 1- Elnath. 6471. How Is the correction for a refractionerror applied to 2-Pollux. the HS (height sighted)? 3-Aldebaran. 1--Subtracted for Moon observations only. 2-Subtracted for all celestial observations. 6480. The star at the end of the handle of the Little Dipper 3-Added for Sun, Moon, and the planets. (URSA minor) is 1-Dubhe. 6472. When observing the Moon HS, which correctionsare 2-Kochab. always additive? 3-Polaris. 1--Index. 2-Parallax. 6481. The star at the tail of Scorpius (the scorpion) Is 3- Refraction. 1-Shaula. 2-Antares. 6473. When observing the Moon HS, whichcorrection is 3-Nunki. always subtracted? 1-Index. 64112. To determine latitude by an observation of Polaris, it 2-Parallax. is necessary to adjust the HO altitude 3-Refraction. 1-to the altitude of the poles. 2-for erratic orbit of Polaris. 6474. Why is the Intercept method usedto plot celestial fixes? 3-for change In LHA of Aries. 6483. The correction used during a Polaris observation Is 1-It provides a rapid means of computing theobservations. 2-It eliminates the need to correct for precision. 1-0 correction. 3-The subpoint of most bodies would betoo far to plot on 2-motion of the body. most aeronautical charts. 3-index error. 6475. What measurement does the intercept method 6484. Which of the listed planets is most often used fora provide when determining an LOP fora celestialfix? celestial observation? 1-Nautical miles between the actual circle ofequal altitude 1-Mercury. and that of the assumed position. 2-Uranus. 2- Nautical miles between the position andthe celestial 3-Pluto. body's nadir. 3-The distance In nautical miles between the positionand 6485. Which planetismost often used forcelestial the celestial body's subpoint observations?

6476. Noonday fixes (local apparent noon)can best be 1-Uranus. obtained at 2 -Mars. a-Pluto. 1-lower latitudes. 2-middle latitudes. 6486. The celestial reference lines that are counterparts of 3-higher latitudes. parallels of latitude are called 1-declination circles. 2-hour circles. 3-diurnal circles.

98 108 6467. At what location are all celestial bodice circumpolar? 6495. Time of transit refers to 1-30'. 1-the altitude of a body above the observer's celestial 2-80'. horizon. 3-Either pole. 2-the time when a body passes the absentees meridian. 3-when the Sun passes overhebd in the sky. 44811. At what location are none of the celestial bodies circumpolar? 6496. A 1-hour time zone is equal to how many degrees or minutes of longitude on the Earth's surface? 1-The Equator. 2-30'. 1 -1 5'. 3-00'. 2-1'. 3-15 minutes. 6496. What is the name of the celestial counterpart for longitude? 8497. How many degrees of longitude does the mean Sun travel in 3 hours 20 minutes? 1--Dedination. 2-Hour cdes. 1-45'. 3-Diurnal circles. 2-50'. 3-55'. 6490. What Is the name of the point directly above the observer's position on the celestial sphere? 64911. How many degrees of longitude does the mean Sun travel in 2 hours 40 minutes? 1 -Na dr. 2-Zenith. 1-35'. 3- Antes. 2-40'. 3-45'. 6491. From which publication can the GHA of the Sun, Moon, planets, and Mee be obtained? 6499. Sidereal time is defined as 1-41.O. Pub. No. 218, Ak Navigation. 1-*..ae measured by reference to the upper branch of the 2-41.O. Pub. No. 249, Sight Reduction Tables, Volume I. first point of Aries. 3-Ak Almanac. 2-when the Sun passes from north to south declination across the equinoctial. MU. How is the first point of Aries defined? 3-time measured from the Greenwich Meridian to the 1--Point where the Sun crosses the observer's upper observer's lower branch. branch. 6500. Where should the course be measured when plotting 2-Point r.ttr: itso Sun appears to cross the celestial on a Lambert Conformal Chart? Equator from non?, to south. 3-Point where the Sun aooears to cross the celestial 1-Any longitude. Equator from south tc, north. 2-Mid-longitude. 3-Mid-latitude. 6492. What is the LHA of a celestial body using the following information? 6601. On whichr.. Art does a straight line represent a rhumb line? Longitude of the observer 85' E OHA Arles. 3r 1-Mercator. SHA of an observed body 47' 2-Lambert conformal. 1-85'. 3-Stereographic. 2-150'. 6502. True airspeed Is defined as the 3-430'. 1-reading taken from the airspeed indicator. MK What is the LHA of a celestial body using the 2-Indicated airspeed corrected for pitot-static error. foNowing information? 3-calibrated or equivalent airspeed corrected for temperature and pressure altitude. Longib.kte of the observer 35' W GHA Aries. 95' 6503. Calibrated airspeed is defined as the SHA of an observed Sod), 45' 1-indicated airspeed corrected for pitot-static error. 1-45'. 2-indicated shined corrected for compressibility. 2-105'. 3-calibrated or equivalent airspeed corrected for tempera- 3-140'. ture and pressure altitude.

109 99 6104. Track is defined as the 6511. The following symbol represents 1intended horizontal direction of travel of an aircraft over the ground. 2horizontal component of the actual path of an aircraft MK the ground. 9horizontal component of the intended path of the aircraft 4 comprisktg both direction and magnitude.

6106. An AP (air position) Is defined as 1a DR position. 1a point on the Earth established by keeping an accurate 2--an airr position. account of time, groundspeed, and track since the last 3--a fix. known position. 2c -' accurate position determined by electronic equip- 8512. The following symbol represents ment 3the location of an aircraft In relation to the akmass surrounding it 8108 The following symbol represents T>»

1--an air vector. 2an air position. » 3a wind vector. j 8513. The following symbol represents

1an air position. 2a ground track 3a wind vector. 8107. How is Doppler groundspeed determined? Lo i 1By compering the frequency from the forward beam with 1a DR position. the frequency from the aft beam. 2--an air vector. 2By the automatic astrotracker 3a wind vector. 3By comparing electronic signals sent from a master stationwiththose received from a slavestation. 8514. With a relative bearing of 095', a compass heading of 303', and a local variation of 2' west, what is the true NNW The Doppler system provides bearing TO the NDB? 1true *speed. 2true sir temperature. FOR (MAGNETIC) N 30 80 E 120150 3drift angle and groundspeed. STEER (COMPASS) 0 28 57 88117 148 FOR (MAGNETIC) S 210240 W300330 6606. Which le a basic component of an INS? STEER (COMPASS) 180212243274303332 1Antenna. 2Accelerometer. 3Amplifler. 1-033'. 2-o3r. 1110. The key to a successful Inertial system Is 3-213'. 1absolute accuracy In measuring horizontal acceleration. 2ability to maintain a 'constant reference to true north. 3eynchronization of signals.

110 . 100 0615.With a relative bearing of 120% a compass heading 6516. A Schuler-tuned inertial system of 21r, and a local variation of r west, what is the this 1dampens drift input bearing TO the NW? 2measures horizontal acceleration. 3prevents errors caused by gravity. N 30 80 E 120150 0 28 57 88117 148 6517. When the star Alpheratz is on the upper branchof an S 210240 W300 330 observer's meridian, what isthe Local Sidereal Time? 180212243274303 332 1-0000. 2-0600. 3-1200. 1-141% 2-15r. 3-321'. Flight Navigator Problem No.1,Part 1 Jacksonville, Florida, to Bermuda island Preflight Planning. NOTE: Flight navigator applicants must provide theirlwn plotters, dividers, computers, flight logs, and celestial forms. They may provide their own charts (GNC 9 or equivalent)or may use a copy of the charts, figures 154, 155, 156, 157 and Celestial Charts, figures 134 through 153. The testmonitor will assure that the logs, forms, and charts are free of markings that would compromise the test. The monitor will also determine thatthe applicant's computer is acceptable.

Instructions for Preflight Planning Problem No. 1, Part1..

1. Zero deviation will be used, i.e.,compass heading and magnetic heading are the same.

2. Preflight a trip from Jacksonville, Florida, VORTAC(30'27'N-081'33'W) to Bermuda VOR (32'21'N-064'41'W) via direct route. Estimated time of departure (EDT) is 2100Z,September 19, 1978. The flight is planned for FL190 and 200 KTAS.

3. Winds aloft are forecast as follows:

a. 30630'N-081'00'W 200',30 knots. b. 31'00'N-078'30'W 225',35 knots. c. 31'00'N-076600'W 245',20 knots. d. 32'00'N-071'30'W 285',30 knots. e. 32'00'N-069'00'W 305',35 knots. f. 32'00'N-000'30'W 325',40 knots.

4. Using the forricast winds given in item 3, developa preflight 1.4 for the following legs: a. Jacksonville VORTAC to 0806001N, b. 080'00'W to 077'30'W. c. 077'30'W to 075'00'W. d. 075'00W to 072'30'W. e. 072'30W to 070'00'W. I. 070°00'W to 067'30'W. 9 067'30'W to Bermuda VOR.

5. Answer questions 6518 through 6521 by referringto your preflight log and calculations.

6518. (Refer to instructions 1 through 5 for Part 1.) Whatis 6520. (Refer to instructions 1 through 5 for Part 1.) What is the magnetic heading shown on the preflightlog for the leg the preflight ETE from Jacksonville VORTAC to Bermuda from 077'30'W to 075'00'W? VOR? 1-085'. 1-3 hours 56 minutes. 2-090'. 2-4 hours 03 minutes. 3-095'. 3-4 hours 06 minutes.

6519. (Refer to instructions 1 through 5 for Part1.) What is 6521. (Refer to instructions 1 through 5 for Part 1.) What is the preflight groundspeed for the leg from072'30'W to the preflight distance from Jacksonville VORTAC to Ber- 070'00'W? muda VOR? 1-228 knots. 1-852 NM. 2-232 knots. 2-860 NM. 3-237 knots. 3-868 NM.

. 112102 Flight Navigator Problem No. 1, Part 2 Jacksonville, Florida, to Bermuda island En Route.

Instructions for En Route Planning Problem No. 1, Part 2:

1. See figures 134 through 153 for required celestial data and tables.

2. Alter headings, when instructed, at specified fix positions.

3. Navigation aids:

a. Jacksonville VORTAC 30 °27'N 081°34'W. b. Johns Island NDB 32'42'N 080'00'W. c. Bermuda VOR 32'21'N 064°42'W. d. Grand Bahama NDB 26°38'N 078°22'W.

4 Complete the following scenario and answer the en route questions by referring to your preflight logs and calculations (Part 1)

a. Depart Jacksonville VORTAC at 2130Z, level 19,000 feet, 200 KTAS, magnetic heading 089°

(1) Pressure altitude 19,025 feet. (Assume altitude readings are taken over water.) (2) Absolute altitude 20,150 feet (Assume altitude readings are taken over water.)

b. Compute an ETA for crossing the 80°00'W longitude on the first leg using preflight winds.

c. Determine position at 22202 based on the following data:

(1) Johns Island (JZI) NDB indicates a 319* magnetic bearing to the station. (2) Pressure altitude 19,000 feet (3) Absolute altitude 20,285 feet. (4) The Sun is observed with an HS of 10°45'.

d. After heading to next position (31'24'N 075°00'W) from the 2220Z fix position (disregard the DR position).

e. Determine the position at 2310Z based on the following data:

(1) Polaris is observed with an HS of 31'19' at 2306Z. (2) Venus is observed with an HS of 16°33' at 2310Z. (3) Grand Bahama (GBN) NDB indicates a 223° magnetic bearing to the station. (4) Pressure altitude 19,000 feet. (5) Absolute altitude 20,575 feet.

(NOTE: Expect jetstream influence on this leg.)

f. After heading to next position (31°55'N 070°00'W) from the 2310Z position (disregard the DR position).

g. Determine the position at 0000Z based on the following data:

(1) Alpheratz is observed with an HS of 28°11' at 0000Z. (2) Allcald is observed with an HS of 27'30' at 0004Z. (3) Pressure altitude 18,900 feet. (4) Absolute altitude 20,760 feet

(NOTE: Expect jetstream influence on this leg.)

h. Alter heading to Bermuda VOR (32°21'N 064°42'W) from the 0000Z fix position (disregard the DR position).

I Determine the position at 0050Z based on the following data:

(1) Polaris is observed with an HS of 3118' at 0046Z. (2) The upper limb of the Moon is observed with an HS of 03'42' at 00502. (3) Bermuda (NWU) NDB Indicates 059° MB to the station.

j. After heading to Bermuda VOR (32'21'N 064°42'W from the 0050Z fix position (disregard the DR position).

103 :".;', .1 1 3 k. Complete the flight lag from the 0050Z fix positionto Bermuda VOR.

(NOTE: This Is an academic problem; therefore, the windvelocity, direction, and atmospheric pressure may not be typical for the area and the time of year.)

5. Answer questions 8522 through 8535 by referring to thein-flight log and calculations.

8522. (Refer to instructions 1 through 5 for Part 2.) After 6529. (Refer to instructions 1 through 5 for Part 2.) What is departing over the Jacksonville VORTAC, what is the ETA the position of the 0000Z fix? at 30642'N - 080'00'W? 1-31'25'N - 089'32'W. 1-21531 2-31'37'N - 069'40'W. 2-21581 3-31'51'N - 089'42'W. 3-22011 6530. (Refer to instructions 1 through 5 for Part 2.) What is $623. (Refer to Instructions 1 through 5 for Part 2.) What is the wind between the 2310Z fix and the 0000Z fix? the position of the 2220Z fix? 1-240', 99 knots. 1-31'12/4 - 078'17'W. 2-238', 88 knots. 2-31'09'N - 078'12'W. 3-251', 105 knots. 3-31'17'N - 078'23'W. 6531. (Refer to instructions 1 through 5 for Part 2.) What is MAL (Refer to instructions 1 through 5 for Part 2.) What is the ETE between the 0000Z fix and Bermuda VOR the true come from the 2220Z fix to the next position, 32'21'N - 084'42'W? 31'24'N - 075'00'W? 1-50 minutes. 1-078'. 2-55 minutes. 2-079'. 3-60 minutes. 3-086'. 6532. (Refer to instructionsthrough 5 for Part 2.) What is 111125. (Refer to Instructions 1 through 5 for Part 2.) What is the position of the 0050Z fix? the distance from the 2220Z fix to the next position, 31'24'N - 075'00'W? 1-31'31'N - 065'48'W. 2-31°40'N -- 065'32'W. 1-159 NM. 3-31'37'N - 065'40'W. 2-189 NM. 3-175 NM. 6533. (Refer to instructions 1 through 5 for Part 2.) What is the groundspeed between the 0000Z fix and the 0050Z fix? $SA (Refer to Instructions 1 through 5 for Part 2.) What is the position of the 2310Z fix? 1-239 knots. 2-244 knots. 1.-31'33'N - 074'00'W. 3-250 knots. 2-3146'N - 074'15'W. 3-31'58'N - 074'10'W. 6534. (Refer to instructions 1 through 5 for Part 2.) What is the true heading between the 0050Z fix and the Bermuda 5527. (Refer to instructions 1 through 5 for Part 2.) What is VOR? the distance between the 2220Z fix and the 2310Z fix? 1-041'. 1-211 NM. 2-048'. 2-217 NM. 3-059'. 3-222 NM. 6535. (Refer to instructions 1 through 5 for Part 2.) What is UK (Refer to instructions 1 through 5 for Part 2.) What is the ETA at Bermuda VOR from the 0050Z fix? themagneticheadingbetweenthe2310Zfixand 31'55'N - 070'00'W? 1-0051Z. 2-0058Z. 1-105'. 3-0107Z. 2-110'. 3-118'.

i 114 Plight Navigator Problem No. 2, Part 1 Corpus Christi, Texas to Key West, Florida Preflight Planning.

NOTE:Flight navigator applicants must provide their own plotters, dividers, computers, flight logs, and celestial forms. They may provide their own charts (GNC 9 or equivalent) or may use a copy of the charts in figures 154, 155, 158, 157, and Celestial Charts, figures 134 through 153. The test monitor will assure that the logs, forms, and charts are free of markings that would compromise thetest. The monitor willalso determine that the applicant's computer is acceptable.

Instructions for Preflight Planning Problem No. 2, Part 1:

1. Zero deviation will be used, i.e. compass heading and magnetic heading are the same.

2. Preflight a trip from Corpus Christi, Texas, VORTAC (27'54'N 097'28'W) to Key West, Florida, VORTAC (24'35'N 081'481W) via direct route. Estimated time of departure (EDT) is 0900Z, September 20, 1978. The flight is planned for FL190 and 200 KTAS.

3. Winds aloft are forecast as follows:

a. 27'30'N 098'00'W 310',25 knots. b. 27'30'N 092'30'W 290',30 knots. c. 28'00'N 089'00'W 270',35 knots. d. 25'30'N 088.00'W 260',35 knots. e. 25'00'N 083'30'W 250',40 knots.

4. Using the forecast winds given in item 3, develop a preflight log for the following legs:

a. Corpus Christi VORTAC to 095'00W b. 095'00'W to 09230'W. c. 092'30'W to 090'00'W. d. 090'00'W to 087'30'W. e. oerww to 085'00'W. f. 085'00'W to Key West VORTAC.

5. Answer questions 6536 through 6539 by referring to the preflight log and calculations.

4536. (Refer to instructions 1 through 5 for Part 1.) What is 6533. (Refer to instructions 1 through 5 for Part 1.) What is the magnetic heading shown on the preflight log/form for the preflight ETE from Corpus Christi VORTAC to Key West the leg from 092'30'W to the 090'00'W en route to Key VORTAC? West VORTAC? 1-3 hours 46 minutes. 1-092'. 2-3 hours 51 minutes. 2oa. 3-3 hours 55 minutes. 3-103'. 6539. (Refer to instructions 1 through 5 for Part 1.) What is 11637. (Refer to instructions 1 through 5 for Part 1.) What is the preflight distance from Corpus Christi VORTAC to Key the preflight groundspeed for the leg from 090°00'W to West VORTAC? 087'30'W longitude en route to Key West? 1-888 NM. 1-225 knots. 2-872 NM. 2-229 knots. 3-877 NM. 3-234 knots. Flight Navigator Problem No.2,Part 2 Corpus Christi, Texas to Key West, Florida En Route. Instructions for En Route Planning Problem No.2, Part 2:

1. See figures 134 through 153 for required celestialdata and tables.

2. Alter headings, when Instructed, at specified fixpositions. 3. Navigation skis:

a. Corpus Christi VORTAC 27'54'N 097°26W. b. Brazos Santos NDB 26'04'N 097°09W. c. Leeville VORTAC 29°10'N 090°06W. d. Key West VORTAC 24'35'N 081°48'W. e. Sarasota VORTAC 27'23'N 082°33'W.

4. Complete the following scenario andanswer the en route questions by referring to your preflight logs and calculations (Part2).

a. Depart over Corpus Christi VORTAC at 0930Z,level 19,000 feet 200 KTAS, magnetic heading 091°.

(1) Pressure altitude 19,000 feet. (Assume altitude readings are taken over water.) (2) Absolute altitude 20,470 feet (Assume altitude readings are taken over water.)

b. Compute an ETA for the 095°00'W positionon the first leg using preflight winds.

c. Determine the position at 1010Z based on the followingdata:

(1) The upper limb of the Moon is observed withan HS of 70'34' at 1006Z. (2) Jupiter is observed with an HS of 27°29' at 1010Z. (3) Brazos Santiago NOB indicates a 235' magneticbearing to the station. (4) Pressure altitude 19,060 feet (5) Absolute altitude 20,370 feet

d. Alter heading to next position (26°32'N 090°00'W) from the 1010Z fix position (disregard the DR position). e. Determine the position at 1100Z basedon the following data:

(1) Polaris is observed at 1100Z with an HS of 27°44'. (2) Pressure altitude 19,060 feet. (3) Absolute altitude 20,300 feet (4) The RMI indicates the Leeville VOR 202magnetic radial. f. Alter heading to the next position (28°00'N 087°30W) from the 1100Z fix position (disregard the DR position). g. Determine the position at 1150Z basedon the following data:

(1) Dubhe is observed with an HS of 28'45' at 1146Z. (2) Hamal is observed with an HS of 38°2W at 1150Z. (3) Sirius is observed with an HS of 45°38' at 1154Z. (4) Pressure altitude 19,150 feet. (5) Absolute altitude 20,400 feet.

h. Alter heading to the next position (25°23'N 085°00'W) from the 1150Z fix position (disregard the DR position).

I. Determine the position at 1240Z basedon the following data:

(1) The upper limb of the Moon is observed withan HS of 31°03' at 1240Z. (2) The Sun is observed with an HS of 16'53'at 1244Z. (3) Pressure altitude 19,150 feet (4) Absolute altitude 20,825 feet. (5) The RMI indicates the Sarasota VOR 229 magneticradial.

J. Alterheading tothe1( sy West VORTAC from the 1240Zfixposition(disregardthe DR position). k. Complete the flight log from the 1240Z fix to the KeyWest VORTAC.

106 116 (NOTE:This is an academic droblem; therefore, the wind velocity, direction, and atmospheric pressure may not be typical for the area and the time of year.,

5. Answer questions 6540 through 6553 by referring to thein-flight log and calculations.

8540. (Refer to instruction 1 through 5 for Part 2.) After 6547. (Refer to instructions 1 through 5 for Part 2.) What is &pink over the Corpus Christi VORTAC, what Is the ETA the position of the 1150Z fix? over 27'30'N - 095'00W? 1-28'15'N - 087'42'W. 1-09561 2-26'27'N - 087'53'W. 2-10001 3-28'33'N -- 087'57'W. 3-10061 654$. (Refer to instructions 1 through 5 for Part 2.) What is 041. (Refer to instructions 1 through 5 for Part 2.) What is the wind between the 1100Z fix and the 1150Z fix? the position of the 1010Z fix? 1-252', 30 knots. :,- 1-27'03'N - 094'36W. 2-260', 22 knots. 2-27'11'N - 094655'W. 3-262', 25 knots. 3-27'24'N - 094'29'W. 6549. (Refer to instructions 1 through 5 for Part 2.) What is 6542. (Refer to instructions 1 through 5 for Part 2.) What is the ETE between the 1150 for and the next position, the true course from the 1010Z fix to the next position, 25623'N - 085'00'W? 26'32'N -090'00V? 1-40 minutes. 1-091'. 2-45 minutes. 2-094'. 3-49 minutes. 3-098'. 6550. (Refer to instructions 1 through 5 for Part 2.) What is 6643. (Refer to instructions 1 through 5 for Pert 2.) What is the position of the 1240Z fix? the distance from the 1010Z fix to the next position, 2812N - 090600°N? 1-25'34'N - 084'33W. 2-25'45'N - 084'43'W. 1-257 NM. 3-25'52'N - 084'52'W. 2-268 NM. 3-273 NM. 6551. (Refer to instructions 1 through 5 for Part 2.) What is the groundspeed between the 11502 fix and the 1240Z fix? 6544. (Refer to instructions 1 through 5 for Part 2.) What is the position of the 1100Z fix? 1-211 knots. 2-218 knots. 1-27'09'N - 091'03W, 3-224 knots. 2-27'05'N - 091'17W. 3-28659'N - 091'09W. 6552. (Refer to instructions 1 through 5 for Part 2.) What is the true heading between the 1240Z fix and the Key West 6545. (Refer to instructions 1 through 5 for Part 2.) What is VORTAC? the distance between the 1010Z fix and the 1100Z fix? 1-120'. 1-190 NM. 2-125'. 2-204 NM. 3-130'. 3-219 NM. 6553. (Refer to instructions 1 through 5 for Part 2.) What is 6546. (Refer to instructions 1 through 5 for Part 2.) What is the ETA to the Key West VORTAC from over the 1240Z fix? themagneticheadingbetweenthe1100Zfixand 26'00'N -0e7'30v1? 1- 1332Z. 2-1340Z. 1-ow. 3-1345Z. 2-ow. 3-102'.

117 107 APPENDIX 1

-o- 118 Appendix 1 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION

SUBJECT MATTER KNOWLEDGE CODES

To &denim the knowledge area in which a particular questionwas incorrectly answered, compare the subject matter code(s) on AC Form 8080-2, Airmen Written Test Report, to the subject matter outline that follows. The total number of test items missed may differ from the number of subject matter codes shownon the AC Form 8080-2, since you may have missed more than one question In a certain subject matter code.

FAR 1 Definitions and Abbreviations FAR 71 Designation of Federal Airways, Area Low Routes, Controlled Airspace, and A01 General Definitions Reporting Points A02 Abbreviations and Symbols A60 General FAR 23 Airworthiness Standards: Normal, Util- A61 Airport Radar Service Areas ity, and Acrobatic Category Aircraft FAR 73 Special Use Airspace A10 General A70 General A71 FAR 4$ Maintenance,PreventiveMaintenance, Restricted Areas Rebtdiding and Alteration A72 Prohibited Areas

A15 General FAR 75 Establishment of Jet Routes and Area A16 Appendices High Routes

A80 General FAR Si Certification:Pilots and Flight instructors FAR 77 Objects AffectingNavigable Airspace A20 General A21 Aircraft Ratings and SpecialCertificates A90 General A22 Student Pilots A23 Private Pilots FAR 91 General Operating Rules A24 Commercial Pilots B01 General A25 Airline Transport Pilots B02 Flight Rules A28 Flight Instructors B03 Maintenance, Preventive Maintenance, and A27 Appendix k Practical Test Requirements Alterations for Airline Transport Pilot Certificates and B04 Large and Turbine-Powered Multiengine Air- Associated Class and Type Ratings planes A28 Appendix B:Practical Test Requirements B05 Operating Noise limits for Rotorcraft Airline Transport Pilot Certifi- B06 Appendix A:Category II Operations cates with a Helicopter Class Rating and Manual, Instruments, Equipment, and Main- Associated Type Ratings tenance

FAR $3 Certification: Flight Crewmembers Other FAR 103 Ultralight Vehicles Than Plots CO1 General A30 General CO2 Operating Rules A31 Flight Engineers A32 Flight Navigators FAR 10$ Airplane Operator Security

FAR 56 Certification: Airmen Other Than Flight C10 General Croy/members FAR 121 Certification and Operations:Domestic, MO General Flag and Supplemental Air Carriers and A41 Aircraft Dispatchers Commercial Operators of Large Aircraft

FAR Medical Standards and Certification 001 General 002 Certification Rules for Domestic and Flog A50 General Air Carriers A61 Certification Procedures 103 CertificationRules for SupplementalAir Carriers and Commercial Operators

1 119 Appendix 1 004 Rules GoverningallCertificateHolders E09 Airplane Performance Operating Limitations Under This Part E10 Maintenance, Preventive Maintenance, and D05 Approval of Routes:Domestic and Flag Air Alterations Carriers E11 Appendix A:Additional Airworthiness D06 Approval of Areas and Routes for Supple- Standards for 10 orMore Passenger Air- mental Air Carriers and Commercial Opera- planes tors E12 Special Federal Aviation Regulations SEAR D07 Manual Requirements No. 36 DOB Aircraft Requirements E13 Special Federal Aviation Regulations SFAR 009 Airplane Performance Operating Limitations No. 38 D10 Special Airworthiness Requirements D11 Instrument and Equipment Requirements FAR143 D12 Maintenance, Preventive Maintenance, and Certification:Ground Instructors Alterations F01 General 013 Airman and Crewmember Requirements D14 Trainklg Program US HMR 172 D15 Crewmember Qua lifkations Hazardous Materiels Table 016 Aircraft Dispatcher Qualifications and Duty F02 General Time Limitations:Domestic and Flag Air Carriers US HMR 175 D17 Right Time Limitations and Rest Require- Materials Transportation Bureau Hazard- ous Materials Regulations (HMR) ments:Domestic Air Carriers 018 Flight Time Limitations:Flag Air Carriers GO1 General Information andRegulations D19 Flight Time Limitations:Supplemental Air G02 Loading, Unloading, and Handling Carriers and Commercial Operators G03 Specific Regulation Applicable According to 020 Flight Operations Classification of Material D21 Dispatching and Flight Release Rules D22 Records and Reports NTSB830 Rules Pertaining to the Notification and D23 Crewmember Certificate:International D24 Special Federal Aviation Regulation SFAR Reporting of Aircraft Acddents or Inci- No. 14 dents and Overdue Aircraft, and Prsess vatlon of Aircraft Wreckage, Mali, Cargo, and Records FAR 125 Certification and Operations: Airplanes Having a Seating Capacity of 20 or More G10 General Passengers or a Maximum Payload Ca- G11 InitialNotificationofAircraftAccidents, pacity of 8,000 Pounds or More Incidents, and Overdue Aircraft G12 Preservation of Aircraft Wreckage,Mail, D30 General Cargo, and Records D31 Certification Rulesand Miscellaneous Re- G13 Reporting of Aircraft Accidents, Incidents, quirements and Overdue Aircraft D32 Manual Requirements 033 Airplane Requirements AC61-23 D34 Special Airworthiness Requirements Pilot's Handbook ofAeronautical Knowl- D35 Instrument and Equipment Requirements edge D36 Maintenance H01 Principles of Flight D37 Airman and Crewmember Requirements H02 Airplanes and Engines D36 Flight Crewmember Requirements H03 Flight Instruments D39 Flight Operations H04 Airplane Performance D40 Flight Release Rules H05 Weather D41 Records and Reports H06 Basic Calculations Using Navigational Com- puters or Electronic Calculators FAR 135 Air Taxi Operators and Commercial Op- H07 Navigation erators H08 Flignt Information Publications H09 Appendix 1:Obtaining FAA Publications E01 General E02 Flight Operations AC E03 Aircraft and Equipment 91-23 Pliers Weight and Balance Handbook E04 VFR/IFR Operating Limitations and H10 Weight andBalance Control Weather Requirements H11 Terms and Definitions E05 Flight Crewmember Requirements H12 Empty Weight Center of Gravity E00 Flight Crewmember Flight Time Limitations H13 Index and Graphic Limits and Rest Requirements H14 Change of Weight E07 Crewmember Testing Requirements H15 Control of Loading General Aviation E08 Training H16 Control of Loading Large Aircraft 2 .120- Appendix 1 AC 60-14 Aviation Instructor's Handbook Gyroplane Flight Training Manual

H2O The Learning Process H90 Gyroplane Systems H21 Human Behavior H91 Gyroplane Terms H22 Effective Communication H92 Use of Flight Controls (Gyroplane) H23 The Teaching Process H93 Fundamental Maneuvers of Flight (Gyro- H24 Teaching Methods plane) H25 The Instructor as a Critic H94 Basic Flight Maneuvers (Gyroplane) H26 Evaluation H27 Instructional Aids AC 61-27 Instrument Flying Handbook H30 FlightInstructor Characteristics and Re- 101 Training Considerations sponsibilities IC?. Instrument Flying:Coping with Illusions in H31 Techniques of Flight Instruction Flight H32 Planning Instructional Activity 103 Aerodynamic Factors Related to Instrument H40 Aircraft Maintenance Instructor Characteris- Flying tics and Responsibilities 104 Basic Flight Instruments H41 Integrated Job Training 105 Attitude Instrument Flying Airplanes H42 Planning Aircraft Maintenance Instructional 106 Attitude Instrument Flying Helicopters Activities 107 Electronic Aids to Instrument Flying H43 Appendix 108 Using the Navigation Instruments 109 Radio Communications Facilities and Equip- AC 61-21 Flight Training Handbook ment 110 The Federal Airways System and Controlled H50 Introduction to Flight Training Airspace H51 Introduction to Airplanes and Engines 111 Air Traffic Control H52 Introdson to the Basics of Flight 112 ATC Operations and Procedures H53 The Elect and Use of Controls 113 Flight Planning H54 Ground Operations 114 Appendix:InstrumentInstructorLesson H55 Basic Flight Maneuvers Guide Airplanes H56 AirportTrafficPatternsand Operations 115 Segment of En Route Low Altitude Chart H57 Takeoffs and Departure Climbs H58 Landing Approaches and Landings AC 00-6 Aviation Weather H59 Faulty Approaches and Landings 120 The Earth's Atmosphere H60 Proficiency Flight Maneuvers 121 Temperature H61 Cross-Country Flying 122 Atmospheric Pressure and Altimetry H62 Emergency Flight by Reference to Instru- 123 Wind ments 124 Moisture, Cloud Formation, and Precipitation H63 Night Flying 125 Stable and Unstable Air H64 Seaplane Operations 126 Clouds H65 Transition to Other Airplanes 127 Air Masses and Fronts H66 Principles of Flight and Performance Char- 128 Turbulence acteristics 129 Icing 130 Thunderstorms AC 61-13 Basic Helicopter Handbook 131 Common IFR Producers 132 High Altitude Weather H70 General Aerodynamics 133 Arctic Weather H71 Aerodynamics of Flight 134 Tropical Weather H72 Loads and Load Factors 135 Soaring Weather H73 Function of the Controls 136 Glossary of Weather Terms H74 Other Helicopter Components and Their Functions AC 00-45 Aviation Weather Services H75 Introduction to the Helicopter Flight Manual 40 The Aviation Weather Se vice Program H78 Weight and Balance 41 Surface Aviation Weather Reports H77 Helicopter Performance 42 Pilotand Radar Reports andSatellite H78 Some Hazards of Helicopter Flight Pictures H79 Precautionary Measures and Critical Condi- 43 Aviation Weather Forecasts tions 44 Surface Analysis Chart H80 Helicopter Flight Maneuvers 45 Weather Depiction Chart H81 ConfinedArea,Pinnacle, and Ridgeline 48 Radar Summary Chart Operations 47 Significant Weather Prognostics H82 Glossary 48 Winds and Temperatures Aloft

3 121. Appendix 1

149 Composite Moisture Stability Chart J57 Drugs and Flying 150 Severe Weather Outlook Chart J58 Carbon Monoxide 151 Constant Pressure Charts J59 Vision 152 Tropopause Data Chart J60 Night Flight 153 Tables and Conversion Graphs J61 Cockpit Lighting J62 Disorientation (Vertigo) AIM Airman's Information Manual J63 Motion Sickness J01 Air Navigation Radio Aids J64 Fatigue J02 Radar Services and Procedures J65 Noise J03 Airport Lighting Aids J66 Age J04 AirNavigation and ObstructionLighting J67 Some Psychological Aspects of Flying J05 Airport Marking Aids J68 The Flying Passenger J06 Airspace General J07 Uncontrolled Airspace ADDITIONAL ADVISORY CIRCULARS J08 Controlled Airspace J09 Special Use Airspace KO1 AC 00-24, Thunderstorms J10 Other Airspace Areas K02 AC 00-30, Rules of Thumb for Avoiding or J11 Service Available to Pilots Minimizing Encounters with Clear Air Turbu- J12 Radio Communications Phraseology and lence Techniques K03 AC 00-34, Aircraft Ground Handling and J13 Akport Operations Servicing J14 ATC Clearance /Separations K04 AC 00-50, Low Level Wind Shear J15 Preflight K10 AC 20-5, Plane Sense J16 Departure Procedures K11 AC 20-29, Use of Aircraft Fuel Anti-lcing J17 En Route Procedures Additives J18 Arrival Procedures K12 AC 20-32, Carbon Monoxide (CO) Contami- J19 Pilot/Controller Roles and Responsibilities nation in Aircraft Detection and Preven- J20 National Security and Interception Proce- tion dures K13 AC 20-43, Aircraft Fuel Control J21 Emergency Procedures General K14 AC 20-64, Maintenance Inspection Notes J22 Emergency Services AvailabletoPilots for Lockheed L-188 Series Aircraft J23 Distress and Urgency Procedures K15 AC 20-76, Maintenance inspection Notes J24 Two-Way Radio CommunicationsFailure for Boeing B-707/720 Series Aircraft J25 Meteorology K16 AC 20-78, MaL Ainance Inspection Notes J26 Altimeter Setting Procedures for McDonnell Douglas DC-8 Series Aircraft J27 Wake Turbulence J28 K17 AC 20-84, Maintenance Inspection Notes Bird Hazards, and Flight Over National for Boeing B-727 Series Aircraft Refuges, Parks, and Forests K18 AC 20-99, Angsidd and Associated Systems J29 Potential Flight Hazards K19 J30 Safety, Accident, and Hazard Reports AC 20-101, Omega and Omega/VLF Navi- J31 Fitness for Flight gation Systems Approvals for Use in the J32 Type of Charts Available Conterminous United States and Alaska J33 Pilot Controller Glossary K20 AC 20-103, Aircraft Engine Crankshaft Fail- J34 Airport/Facility Directory ure J35 En Route Low Altitude Chart K21 AC 20-106,AircraftInspectionforthe J36 En Route High Altitude Chart General Aviation Aircraft Owner J37 Sectional Chart K22 AC 20-113, Pilot Precautions and Proce- J38 WAC Chart dures to be Taken in Preventing Aircraft J39 Terminal Area Chart Reciprocating Engine Induction System and J40 Standard Instrument Departure (SID) Chart Fuel System Icing Problems J41 Standard TerminalArrival (STAR) Chart K23 AC 20-121, Airworthiness Approval of Air- J42 Instrument Approach Procedures borne Loran-C Systems for Use in the U.S. J43 Helicopter Route Chart National Airspace System K24 AC 20-125, Water in Aviation Fuels AC 67-2 Medical Handbook for Pilots K30 AC 23.879-1, Control System Locks K31 AC 23.1521-1, Approval of Automobile Gas- J50 The Flyer's Environment oline (Autogas) in Lieu of Aviation Gasoline J51 The Pressure is On (Avgas) in Small Airplanes with Reciprocat- J52 HYPode ing Engines J53 Hyperventilation K40 AC 25-4, Inertial Navigation Systems (INS) J54 The Gas in the Body K41 AC 25.253-1, High-Speed Characteristics J55 The Ears K50 AC 29-2,CertificationofTransportation J56 Alcohol Category Rotorcraft

122 4 Appendix 1

1(60 AC 33.85-1, Surge and Stall Characteristics L43 AC 90-88,AirportRadar Service Area of Aircraft Turbine Engines (ARSA) K70 AC 43-9, Maintenance Records L50 AC 914, Wails!, Slush, and Snow on the K71 AC 43-12, Preventive Maintenanoo Runway K80 AC 60-4, Pilot's Spatial Disorientation L51 AC 91-8,UseofOxygen byAviation K81 AC 60-8, Airplane Flight Manuals (AFM), Pilots/Passengers Approved Manual Materials, Markings, and L52 AC 91-13, Cold Weather Operationof Placards - Airplanes Aircraft K90 AC 60-12, Availability of Industry-Develor ad L53 AC 91-14, Altimeter Setting Sources Guidelines for the Conduct of the Biennial L54 AC 91-16. Category II Operations - Gen- Flight Review eral Aviation Airplanes LO1 AC 61-9, PNot Transition Courses for Corn. L55 AC 91-32, Safety In and Around Helicopters pier Single-Engine and Light, Twin-Engine L58 AC 91-42, Hazards of Rotating Propeller Airplanes and Helicopter Rotor Blades 1.02 AC 61.10, Private and Commercial Pilots L57 AC 91-43, Unreliable Airspeed Indications Refresher Courses L58 AC 91-44, Operational and Maintenance L03 AC 61-12, Student Pilot Guide Practices for Emergency Locator Transmit- L04 AC 81-47, Use of Approach Slope Indica- ters and Receivers tors for Pilot Training L59 AC 91-46, Gyroscopic Instruments - Good LO5 AC 61-65, Certification:Pilot and Flight Operating Prac4xus instructors L60 LO6 AC 61.66, Annual Pilot In Command Profi- AC 91.49, General Aviation Procedures for ciency Checks Right in North Atlantic Minimum Navigation Pert( .mane Specifications Airspace L07 AC 8147, Hazards Associated with Spins in Airplanes Prohibited from Intentional Spin- L61 AC 91.50, Importance of Transponder Oper- ning ation and Altitude Reporting L08 AC 61.84, Role of Preflight Preparation L62 AC 91-51,AirplaneDeice and Anti-Ice 1.09 AC 81-89, Pilot Certificates:Aircraft Type Systems Ratings L63 AC 91-53,Noise Abatement Departure L10 AC 81.92, Use of Distractions During Pilot Profile Certification Flight Tests L64 AC 91-55, Reduction of Electrical System L11 AC 81.94, Pilot Transition Course for Self- Failures Following Aircraft Engine Starting Launching or Powered Sailplanes (Motor L65 AC 91-58, Use of Pyrotechnic Visual Dis- gliders) tress Signaling Devices in Aviation L20 AC 67-1, Medical Information for Air Ambu- L66 AC 91-64, Use of Remote Altimeter Settings lance Operators Instrument Approach Procedures L30 AC 90-23, Aircraft Wake Turbulence L67 AC 91-83, Canceling or Closing Right Plans L31 AC 90-34, Accidents Resultingfrom L70 AC 97.1,Runway Visual Range (RVR) Wheelbarrowing in Tricycle-Gear Equipped L80 AC 103-4, Hazard Associated with Sublima- Aircraft tionof Solid Carbon Dioxide (DryIce) L32 AC 90-42, Traffic Advisory Practices at Aboard Aircraft Nontower Airports L81 AC 103-6,Ultra lightVehicle Operations 133 AC 90-45, Approval of Area Navigation Airports, ATC, and Weather Systems for UseintheU.S.National L82 AC 103-7, The Ultra light Vehicle Airs PaoSystem M01 AC 120-12, Private Carriage Versus 1_34 AC 90-48, Pilots' Role. in Collision Avoid- Common Carriage of Persons or Property ance M02 AC 120-27, Aircraft Weight and Balance L35 AC 90-58, VOrl Cimrse Errors Resulting Control from 50 kHz Channel Mis-Selection M03 AC 120-29 Criteria for Approving Category I L36 AC 90-86, Recommended Standard Traffic and Category IILanding Minima for FAR Patterns for Airplane Operations at Uncon- 121 Operators trolled Airports M04 AC 120-32, Air Transportation of Handi- L37 AC 9047, Light Signals from the Control capped Persons Tower for Ground Vehicles, Equipment, and M10 AC 121-6, Portable Battery -Powered Mega- Personnel phones L96 AC 90-79, Recommended Practices and M11 AC 121-24, Passenger Safety Information Procedures for the Use of Electronic Long Briefing and Briefing Cards Range Navigation Equipment M12 AC 121-25, Additional Weather Information: L39 AC 90-82, Random Area Navigation Routes Domestic and Flag Air Carriers L40 AC 90-83, Terminal Control Areas (TCA) M13 AC 121-195, Alternate Operational Landing L41 AC 90-85, Severe Weather Avoidance Plan Distances for Wet Runways; Turbojet Pow- (SWAP) ered Transport Category Airplanes L42 AC 90-87,Helicopter Dynamic Rollover

5 - `123 AC 125-1, Operations of Large Airplanes The Balloon Federation Of America Handbook Subject to Federal Plation Regulations Propane Systems Part 125 M30 AC 135-3, Air nod Operators and Commer- 020 Propane Glossary cial Operators 021 Chemical and Physical Systems M31 AC 135-9, FAR Part 135 Icing Limitations 022 Cylinders M32 AC 135-12, Passenger Information, FAR 023 Unes and Fittings Part 135:Passenger Safety Information 024 Valves Briefing and Briefing Cards 025 Regulators M40 AC 150/5345-28, Precision Approach Path 028 Burners Indicator (PAPI) Systems 027 Propane Syste Schematics M50 AC 20-34, Prevention of Retractable Land- 028 Propane Refers, ices ing Gear Failures M51 AC 20.117,Huards Following Ground Deic- The Balloon Federation Of America Handbook ing and Ground Operations in Conditions Avoiding Power Nne Accidents Conducive to Aircraft Icing 030 Excerpts

American Soaring Handbook Gliders Balloon Right Manual N01 A History of American Soaring 040 Excerpts NO2 Training NO3 Ground Launch N04 Airplane Tow Airship Operations Manual NO5 Meteorology P01 Buoyancy N06 Cross-Country and Wave Soaring P02 Aerodynamics N07 instruments and Oxygen P03 Free Ballooning N06 Radio, Rope, and Wire PO4 Aerostatics N09 Aerodynamics P05 Envelope N10 Maintenance and Repair P06 Car P07 Pant Soaring Flight Manual Gliders P08 Airship Ground Handling P09 Operating Instructions N20 SaNplane Aerodynamics P10 History N21 Performance Considerations N22 Flight instruments International Flight Information Manual N23 Weather for Soaring N2i Medical Factors 001 Passport and Visa N25 Flight Publications and Airspace 002 International NOTAM Availability and Distri- N26 Aeronautical Charts and Navigation bution N27 Computations for Soaring 003 National Security N28 Personal Equipment 004 International Interception Procedures N29 Preflight and Ground Operations 005 Intercept Pattern for identification of Trans- N30 Aerotow Launch Procedures port Aircraft N31 Ground Launch Procedures 006 Flight Planning Notes N32 Basic Flight Maneuvers and Traffic Patterns 007 North Atlantic Minimum Navigation Require- N33 Soaring Techniques ments N34 Cross-Country Soaring 008 North American Routes for North Atlantic Traffic Taming The Gentle Giant Balloons 009 U.S. Aeronautical Telecommunications Services 001 Design and Construction of Balloons 010 Charts and Publications for Flights Outside 002 Fuel Source and Supply the U.S. 003 Weight and Temperature 011 Oceanic Long-Range Navigation Information 004 Right Instruments 005 Balloon Right Tips Aerodynamics For Naval Aviators, NAVWEPS 0040T-110 006 Glossary RO1 Wing and Airfoil Forces Balloon Federation Of America Flight Instructor R02 Planform Effects and Airplane Drag Manual R10 Required Thrust and Power R11 Available Thrust and Power 010 Flight Instruction Aids R12 Items of Airplane Performance 011 Human Behavior and Pilot Proficiency R21 General Concepts and Supersonic Flow 012 TheFlight Check and the Designated Patterns Examiner R22 Configuration Effects 6 124 R31 Definitions X01 Reserved R32 Longitudinel StabiNty and Control Y01 Reserved R33 Dkeo Kona! %bilk and 0 atrol 201 VisualFlightRules Chart Users Guide R94 Lateral StabiNty and Cot.- ol 202 Pilots Guide to IVRS R95 MbosiMneous Stability Problems NOTE Most of the references and study materials fisted in R40 General DefinMons and Structural Requke- these subject matter knowledge codes we available through ments government outlets such as U.S. Government Printing Office R41 Aircraft Loads and Operating Limitations bookstores. AC 00-2, Advisory Circular Cheddiet, transmits R50 Applicationof Aerodynamics toSpecific the status of all FM. AC's (advisory circulars). as well as Problems of Flying FM internal publications and miscellaneous flight intone- don such as AIM, Airport/Facility Directory, written test Transport Airplane Operations Manual question books, practical test standards, and other materiel directly related to a certificate or rating. To obtain a free S01 Reserved copy of the AC 00-2, send your request to T01 Rammed U01 Reserved U.S. Department of Transportation VO1 Reserved Utilization and Storage Section, M-443.2 W01 Reserved Washington, DC 20590

7 125 APPENDIX 2

126 Appendix 2

LEGEND *ESTRUM:01f APPROACH INIOCEDUPIS LO4AITS) SYSTEMS- UNITED STATES led tweeds ligNieg yarn indlessed ips Alf" NO Dloorenn will bees "OWN hilsillikEN littlimiedell *Net A Ns "" pesireyed wish lighting leiter Idendfler indketes sequenced Rushing lights (F) instilled with the epensoch lighting "am e.g.

RUNWAY TOUCHDOWN ZONE AND 6 0 NAVY PARALLEL ROW SIMPUFIED SHORT CENTERLINE WONTING SYSTEMS AND CROSS OAR APPROACn UGHTING SYSTEM CL OMEN 1 11111NIAll wilh OMR" AriptIaM iltliketel Ughs MINIM SSAUt 140 OD CL \.,...... No Iir TOE - Ma 1 _L. lrit TO2 ...... I -r"'" weemom 1: . no AvAitAsuly one/awia In shown bY 1 2 mos NOTE In SKETCH 66. "TDZ/C1 Rwy 1r .., ..... ND APPROACH UOHTINO mem MO low*/ ALS12 LENGTH I300' PEET LENGTH 2400 FEET T, 0.0 .... w...... MEDIUM INTENSITY(MALS end 0 AIR FORCE OVERRUN 1-..: ... = ...E' wm" MAUF) OR SIMPLIFIED SHORT ...... UMW moo k me I, (SSALS end SSALF) una APPROACH LIGHTING SYSTEMS 11,- ...NO ore sr 1111411 IR° 1/4 "r lif , IIUNWA, IlD 7. I ,- HAMM)11101INCIO : 1 4- ' *es .... IF I 1110UINCID LENGTH 1000 FEET -r womm-.-74NAmoms mons PoR i MAOMIALF VISUAL APPROACH MO WITTIWTO ow SLOPE INDICATOR LENGTH 2400/3000 FEET VASI LENGTH 14t6, FUT APPROACH UONTING SYSTEM VAR 2 0 VASA 4 ME.' 6 MEDIUM INTENSITY ..... APPROACH LIGHTING SYSTEM NAI wish Newsy Atiormari ladieeter Ugh% 1 .'"'avi .... MAUS ...., 7' ..... 1 i IMMO 36 ...r. nalK2a6 1___...... -Z..... a. =7-.7 = wawa= .1. VAS 6 VASI 12 k i ÷ ...... T ...? vows .6 mo 1 0 ..... -r In Geo LENGTH 2400 FEET vows ..r T OMNIDIRECTIONAL e sin ..... APPROACH LIGHTING SYSTEM ODALS toA. nat. vsniMML 1PPROACII MR NDICATOR E/1114 STAI/DAED TWIN= CIE/MANCE (High Inseraity) NIOVIDID. LENGTH 2400/3000 FEET D AU LIME MIMI - TOO MON Pm uoons MID SHORT APPROACH LIGHTING SYSTEM ON OWN SLOPI NEAR DONT.VANN I ' AIL MINTS ND - r"...4Lew SALS /SALM I mance 6 (Nigh 10.00 --r L..u... 2:1111Al ANDAWN MON INDICA TM A 11111111101D CROSSING MOW TO SAME AS INNER 1500' OF ALSF1 I. ACCOMODATE IMO 10011D ORMAIO lENOTIS 1500 FUT ANICRAFF.

LEGEND1.InstrumentApproach ProceduresChart (Approach Lighting Systems).

127 MS Men DIM of PAP Rwlziets GENERAL INFORMATION & ASEREVIATIONS * thellades central tower or ATIS operates normonlinuoudy, or non-standard Not Controlled lighting. Oh lenses In naulical mist (met* *hay in statute miles and Runway Visual Range in hundreds of feet). Runway Dimensions in feet. Erse liens in feet Mean Sea Level (MSI). Callings In foal oboes zallthel elevation. Iledials/isearings/heodings/ceunes are magnetic IIIndicates central tower temporarily dosed Usti.

ADP Automatic Direction Finder MAIM Medium Intensity Approach ALS Approach Light System Lighr Systems with RAIL ASP Approach Light System with MAP Missed Approach Point Sequenced Flashing Lights MDA Minimum Descent Attitude APP CON Approach Control Met Medium IMensity Runway lights All Arrival MIS Microwave Landing System ASR/PAR Pubhthed Radar Minimums at MM Middle Marker this Airport NA Not Authorized AMS Automatic Terminal information NOR Non-diredional Radio Beacon Service NM Nautical Mlles AV/05 Automated Weather Observing NoPT No Procedure Turn Required System (Procedure Tan had not be AZ Azimuth executed without ATC clearance) BC Bock Course COALS Omnidirectional Approach light C Cirdirq System CAT Category OM Outer Marker CON Counter Clockwise R Radial Own Channel RA Radio Altimeter setting height CINC DEL Clearance Delivery Radar Required Rader vectoring required CTAP Common Traffic Advisory for this approach Frequency RAII. Runway Alois met k...iketin CW Clockwise DOW OH Decision Heights Nth Radio Beacon DME Distance Measuring Equipment RCLS Runway Centerline light System OR Dead Reckoning NEIL Runway End identifier Ughts MEV Elevation RNAV Area Navigation PAP Final Approach Fix III Runway Point of Intercept(ion) FM Fan Marker MD Runway Remaining Ugh* GM Around Point of interception Runway Touchdown Zone..First 3000' of Runway GS Glide Slope Rwy Runway KM Height Above Airport RVR Runway Visual Range HAL Height Above Landing S Straighhin HAT Height Above Touchdown SALS Short Approach Light System HIRL tegh Intensity Runway Lights SSALR Simplified Short Approach IFI Initial Approach Re Light System with RAIL ICAO Intimation& Civil Aviation SDI Simplified Dkedional Facility Organization TA Transition Attitude IM Inner Marker TAC TACAN inscp Intercept TCH Threshold Crossing Height MT Intersedion (height in feet Above Ground IDA Localize, Type Directional Aid Level) 149 Landing MI Touchdown Zone WIN Lead in light System TDIE Touchdown Zone Mevation DID Low Intensity Runway Lights TDZ /CL Touchdown Zone and Runway LOC Locolizer Centerline Lighting llf Lead Radial. Provides at least MA Touchdown Zone Lights 2 NM (Copt. 1 NM) of lead Its Transition Level to assist in turning onto the %%SI Visual Approach Slope Indicator intermediate/final course VDP Visual Descent Point MALS Medium Intensity Approach WPT Waymire (RNAV) Light System X Radar Only Frequency PILOT CONTROLLED AIRPORT LIGHTING SYSTEMS Available pilot controlled lighting (PCL) systems ore indicated as follows: 1. Approach lighting systems that bear a system identification ore symbolized using negative symbology, e.g.;i11),. 2. Approach lighttng systems that do not beer o system odntification are indicated with a mpgative " b. the name A star (e) Indicates nonitandord PCL, consult Directory/Supplement,g .9* To wive* lights use frequency indicated in the section of the chart with a or the appropriate lighting system identification e.g.. UNKCM 122 II 0

KEY MIKE FUNCTION 7 tines within 5 seconds Highest intensity available 5 times within 3 seconds Medium or lower intensity (Lower RED or RElt-oft, 3 times within 5 seconds Lowest intensity available (Lower REIL or REIL-off)

LEGEND 2.General Information and Abbreviations.

128 2 Appsndlx 2

LEGEND INSTRUMENT APPROACH PROCEDURES (CHARTS)

PLANVIEW SYMBOLS

TERMINAL ROUTES SPECIAL USE AIRSPACE

RResakted W.Wersing Procedure Track 3S gr3° PProhltd A-Pert Missouri Turn Missed Ammo& (Typo dares and ilfal RADIO AIDS TO NAVIGATION Masi Might of turn eerie* 110.1 Underline indkelss No Voice tronsmittai on this 3100 Ner SA NM se OS haqk kfIllomY 043 0 YOE. CI 1101/DME Q TACAN VYORTAC fr"(-14.2 to LOM) Minkeven Altitude NOS PIDI/IDAY 2000 1SS 41101th LOM (Compote Neater at Outer Mrhr) hods. Rouge (13.1)mkop Penetreles Spedal Use Ainpace 411.110 Mather Seam Ig:Z=INILecellze(1,0C/1LIA)Cmurat

HOLDING, PATTERNS SDP Course In Neu of Missed Approach Procedure Dan New NIS Or I.

MLS Approach Azimuth Coverage Arrival Old MICROWAVE Chan 314 Idengior -VCIZ 12. UmNs esti be specified when they desists (MINA 6.20° from Mn sleadard. DAZE fame way be shown. Azimuth 01*(11) REPORTING POINT/FIXES 111.3 Cben IS Y aspetting Net LOC/DME A Nome (Cornpulory) LOCADA/SONSALS Transmitter '(shown when installation U offset from its A Nome (NenCompulsory) itasnection XFin normal position eff the sad of the runway. Womb* (WT) ARC/DMEAINAV Rs Nappint Dote

161111 Radial line and Niue toed Nodal N3116311.30' WW31.30' U611111 112.7 CAP 117.146.2

MINIMUM SAFE ALTITUDE (MSA) WaypoiM Name, Coordinates, 'mammy. identifier, Radial/Distance (PolllifY h w01101111) ileference Peaty Devetion Printery taw Aid ___malady with INS data Nov Aid

LIMA agl LAVA2411

(Arrows on &how circle ideetily wars) MISCELLANEOUS OBSTACLES YOR Chengoover Point Spot Ilevelimi Highest Spot Elevoiion

A Obstacle AA Group of Obseadss AAA Distance not to scale A Highs* doses& ± Doubtful Accuracy ann inkontational Seeming,

LEGEND 3.Instrument Approach Procedures Chart (Planview).

129 LEGEND INSTRUMENT APPROACHPROCEDURES (CHARTS)

PROFILE 204-- Remain within LOM 24gg 10 NM son mow, Outer Marber/FAF Teardrop Turn FAF (nonprecision approaches) Missed Approach Point

2 245k7. ON& OPP* os 3.00 eeGlicaSioPPS Mimed Approach Track Threshold Crossing Height --.401 100 / Glide Slope intercept Altitude Airport Profiles (Primary) (Secondary)

DESCENT FROM HOLDING PATTERN

VOR VOR 1 7 127 WM ,C4 3078-111. 'MC . Nui41, MAP WIT 1 Final Approach Angle for Vertical /ale Computers-... 7 (RNAV Descent) 3.02 ''.

MLS APPROACH Glidepath Altitude at FAF MADEAt- Final Approach Fix (Fall VOR DME MJE 2 2 DAV 3300 ,180°+.16° MLS Glidepoth MLS 0011/L Glidepals 3.0 TCH 30

FACILITIES /FIXES ALTITUDES PROFILE SYMOOLS FM MMandatory Altitude stFinal Approach Fix (FAF)

IM I (for nonprecision approaches) MM 2500 Minimum Aihtude NDII FIX Glide Slope/Oh& Palls Memo OM INT ZiTt5 Maximum Altitude Maude end VOR for precson Unless VTACANORTAC 3000 Recommended Altitude 2400 otherwise indicated the non-prechion final approach altitude h to be WPT maintained until the next fix.

V Visual Descent Point (VD) - Visual Flight Path

LEGEND 4. Instrument Approach Procedures Chart (Profile).

130

4 LEGEND INSTRUMENT APPROACH PROCEDURES (CHARTS)

AIRPORT DIAGRAM/AIRPORT SKETCH

Runways Ea] Ir Helicopter Alighting Areas 0 ffo go Nord Other Than Overruns, Taxiways, Displaced4 Surface Nord SurfaceParking Areas Threshold Negative Symbols used to identify Copier Procedure landing point 11111 0 Runway TDZ elevation TOZE 123 ClosedOozed Under Aimal Surface Runway Total Runway Gradient Runway' Taxiways Construction Contently* 0.R% UP lighhng (shown when runway go:14M exceeds 0.3%) Arresting Gear

rvmdiescianol I Jet Barrier U.S Navy Optical landing system (01S) "CM location is shown because of its height of approximately 7 feet and proximity to edge of runway may create on obstruction for 101110 types REFERENCE FEATURES of aircraft.

Ruildings Approach light symbols are shown on a boons* legend. Airport diagram scales are variable Tanks Two/magnetic North orientation may vary from diagram to diagram. Obstruction A Coordinator velum are shown in l'or b minute were Almon Beacon It month:They ore further broken down into 6 second ticks, within each 1 minute increment.

Runway Positional accuracy wmn ±600 feet unless otherwise tbdor Reflectors noted on the chart

NOTE Control Tower It Airport diagrams that are referenced to the World Geodetic System (WGS) (noted on appropriate It When Control Tower and Rotating Beacon are diagram), may not be compatible with local coordinates ethlocoied, Seam symbol will be used and published in RM. further identified as TWE.

Runway FIELD Runway Gradient REV Identification a 023. 1000 X 200 REV l's. Runway EndElevations164 Runway DimensionsRunway\ Heading Overrun Dimensions (n foot) (Mognetic) (in fool) GENERAL INFORMATION (NOS) SCOPE Airport diagrams are specifically designed to assist in the movement of ground traffic at locations with complex runway/taxiway configurations and provide information for updating Inertial Navigation Systems (INS) aboard aircraft. Airport diagrams are not intended to be used for approach and landing or departure operations. Requisition for the creation of airport diagrams must meet the above criteria and will be approved by the FAA oc DOD on a cassthrcaso bees. MINIMADATA Alternate Minimums not standard. ACivil won refer to tabulation USA/USN /USAF pilots refer to appropriate regulations. Alternate minimums are Not Authorized ANA due to unmonitored facility or absence of weather reporting warms. Takeoff Minimums not standard and/or ODeparture Procedures are published. Refer to tabulation.

LEGEND 5.Instrument Approach Procedures Chart (Airport Diagram).

131

5 . / INSTRUMENT APPROACH PROCEDURE CHARTS RATE OF DESCENT TABLE (ft. per min.)

A rate of descent table is provided for use in planning andexecuting precision descents under known or approximate ground speed conditions. It willbe especially useful for approaches when the localize only is used forcourse guidance.A best speed, power, attitude combination con be programmed whichwill result in a stable glide rate and attitude favorable for executing a landing if minimums exist upon breakout.Care should always be exercised so that the minimum descent altitude and missed approach point are not exceeded.

ANGLE OF GROUND SPEED (knots) DESCENT (deems and tenths) 43 30 60 75 90 103 120 135 150 163 180 2.0 105 160 210 263 320 370 423 475 330 383 633 2.3 130 200 265 330 393 463 330 393 663 730 793 3.0 160 240 320 395 480 555 635 715 795 873 955 3.3 183 280 370 465 353 630 740 833 923 1020 1110 4.0 210 313 423 330 635 740 845 955 1060 1163 1270 4.5 240 353 473 393 715 833 935 1075 1190 1310 1430 5.0 265 395 530 660 795 925 1060 1190 1325 1433 1590 5.5 290 435 580 730 875 1020 1165 1310 1455 1600 1745 6.0 313 475 635 795 955 1110 1270 1430 1590 1745 1905 6.5 345 515 690 860 1030 1203 1375 1350 1720 1890 2063 7.0 370 555 740 925 1110 1295 1480 1665 1850 2035 2220 7.5 395 595 795 990 1190 1390 1585 1785 1985 2180 2380 8.0 425 635 845 1055 1270 1480 1690 1905 2115 2325 2540 8.5 450 673 900 1120 1345 1370 1795 2020 2245 24702695 9.0 475 713 930 1190 1425 1663 1900 2140 2373 2613 2855 9.5 300 730 1003 1233 1305 1733 2005 2253 2510 2760 3010 10.0 330 790 1033 1320 1585 1845 2110 2375 2640 2900 3165 10.5 555 830 1105 1385 1660 1940 221 5 2490 2770 30453320 11.0 380 870 1160 1430 17402030 2320 261 0 29003190 3480 11.3 603 910 1210 1513 1820 2120 24252725 3030 33333633 12.0 630 943 1260 1"9 18902203 2320 2835 3130 3463 3780 / em,, N

LEGEND6. Rate -of- Descent Table.

1326

Appendix 2

Instrument Approach Proadures taw's) INOPERATIVE COMPONENTS OR VISUAL AIDSTAKE

Landing minimums published on instrument approach procedure chartsare based upon full operation cf all components and visual aids associated with theparticular instrument approach chart being used. Higher minimums ore required with inoperativecomponents or visual aids as indicated below. If more than one component is inoperative,each minimum is raised to the highest minimum required byany single component that is inoperative. ILS glide slope inoperative minimumsare published on instrument approach charts as localize, minimums. This table may be amended by notes on the approach chart.Such notes apply only to Wm particular approach category(les)as stated. See legend page for description of components indicated below.

(1) ILS, MLS, and PM Inoperative Approach Increase !WOOS, Component or Aid Category DH Visibility MM MC 50 feet None MM D 50 feet li mile ALSF 1 & Z MALSR, ABCD None li mile & SSALR Not applicable to PAR (2) ILS with visibility minimum of 1,800or 2,000 RVR. MM MC 50 feet To 2400 Milt MM D 50 feet To 4000 IPA ALSF 1 & 2, MALSR, ARCO None To 4000 RVR & SSALR TDZL,Ras ABCD None To 2400 RVR RVR ABCD None To 8 mile

(3) VOR, VOR/DME, VORTAC, VOR (TAC), VOR/DME (TAC), IOC, LOC/DME, LDA, LDA/DME, SDF, SDF/DME, RNAV, qnd ASR Inoperative Approach Increase Increase Visual Aid Category MDA Visibility ALSF 1 & 2, MALSR, ABCD None 14 mile & SSALR SSALS, MALS & ABC None 14 mile ODAIS

(4) NUB

ALSF 1 & 2, MALSR, 14 mile & SSALR MD None 14mile MALS. SSALL ORALS MC 14mile

LEGEND8. Inoperative Components or Visual Aids Table.

134

8 INSTRUMENTAPPROACH PROCEDURES EXPLANATIONOF TERMS lhe Wilted MeleeItemderdler Tenekelbstarment headers, (11.1103) is Me approvedcrawl. ler loneuletleg beemeart oppesachpareedreees.

AIRCRAFT APPROACH CATEGORIES Speeds am basedon 1.3 MusesMs sell moodin the lenders configuration at mexinsumgross lendingweight. An aircraft shall fitin only one asegery.If it is nerameryte maneuver at speeds in mansof the upperlimit of a speed rape fee a category,theMilliOWIIIIIfor Me midhigher category Mould he used 'orexample, on aircraftwhich lolls in Category A, butis drat'g tolad at a speedin mass of 91 knots. should use theapproach CategoryII minimums V when aiding toland. See followingcategorylinikr PM MANEUVERINGTARE INSTRUMENT APPROACH PROCEDURES (CHARTS) VIFR TAKE-OFF MINIMUMS AI4D PROCEDURES Approach A a C D E Category Civil Airports and SelectedMiARTUREhaDEPly Airports CIVILUSERS:FAR 91prescribestake-effrules endestablishes takeoffminima"m follows. Speed 0-90 91.120 121-140 141-165 Abv 165 (1) Aircraft having two engines er less - one stateite mile. (2) Aircraft banns 11019 than two engines - ene-half (Knots) statute miie. MILITARY USERS, Special IFR departure procedures, not published cm SWAIM ifttmoset Dowry* (Sips). and civil take-off minima are included below end ore established to min pints in obstruction avoidance Refer to appropriate service directives for coke -off minimum. AYR/Meteorological Visibifity Comparable Values Airports with IFS take-off minimums other Own standard ere listed below Departure procedures and/er osiNne visibility minimums ore established to assist pilots condor** IFR flight in avoiding obstructions during The fallowingtable shall beused for softening IMI to meteorlogical visibilitywhen IVR is not reportedfor the climb to the minimum worse altitude. Takeoff minimums and departures apply to all runways unless otherwise Adjustment of landing minim may be required- we InoperativeComponents runway of intendedoperation. specified. Altitudes, mks otherwise Indicated, are minimum *Nudes in fete MSL. Table.

RVII (feet) Viability ItVR (feet) Visibility Inches miles) (statute miles) 74 1600 .14 4500...... 1 2400 ...... I/2 soon.. 114 3200 % 6000 4000 %

LANDING MINIMA FORMAT

Inthe enomplewood elweetien is 11711, end runway touchdown zoneelonshen is 1152 INSTRUMENT APPROACH PROCEDURES (CHARTS) Category VNry AircraftApproach IRV" 100's of fest) T AIFR ALTERNATE MINIMUMS (NOT APPUCMILE TO USA/USN/USAF) All minimums In CATEGORY&WM =raina C porenthoses net Standard ahem* minienwns for nonprecision approaches are 800.2 (NOB. VOR, LOC, TACAN, 27s-4,4452y gmluseldeto I1=U 1200-lb Ckril Pilots. LDA, VORTAC, VOR/DME or ASR); for precision approaches 600-2 (11.5 or PAR). Airports within this / , 1440/50 ...,,Mita?. Pd., geographical area that require alternate minimums other than standard or alternate minimums ...... A.S4OC22 1440/24 288 13°"' 25$ 1300-11.'"00.1. ,,,,,"=, with restrictions are listed below. NA - means alternate minimums are not authorized due to bral&-in _Rh Glide SlopeapicuNG 1340-1 1640-1 11640-11h 1740-2 unmonitored facility or absence of weather reporting service. Civil pilots see FAR 91. USA/USN/ 361 (400-1 )i."161 13004 I 461(3004W) 3611600-21f =re USAF pilots refer to appropriate regulations. Rummy zr A MAA Visibility in *ems* Mlles

CORRECTIONS, COMMENTS AND/OR PROCUREMENT

PROCUREFROM: FOR CHARTINGERRORS: FOR CHANCES, ADDITIONS, OR RECOMMENDATIONS ON PROCEDURAL ASPECTS. NationulOcean Service Canton No Ocean kr . NOM, N/C031 Contest Federal Aviation Administration, ATO-256 NOAA.N/0233 Branch 6010 ExecutiveBlvd. 500 independence Avenue. S.W. DieMbution MD. 20737 Itedwfte,MD. 20832 Washington, D.C. 20591 Ilmodele, Telephone(301) 4344993 Telephone Tel -Free800426-3677 klepMne (202) 2674297

Explanation of Terms. LEGEND 9.Instrument Approach Procedures 136 135 DIRECTORY MEND SAMPLE Ip TT f T S' CITY NAME I MINK NAME (OIL)4 E UTC- 1( -40T) 211'32143"1141201117.11 MOININNE 200 II $4 NV 100, JET A OX 1. 2. 3 TPA- 1000(100) AOC CFR Wu ANoe dd. $411410 b 6.44 44 4 44 si e_ M!$* twoocanio(Mr*PFC)$10, 0.110.O1.300 Mk Cl III e AWL Tema IINTIONEIL Rink. T IV Oak 16111011100 (NIN)NV. WI Ilk V1VAINS20 )-0A 33' 1011W. Pals. 010-. NNW IIIIIPt amid 0 MN 31: PAPV2L)-41A 3.1' 10131r. Thea. IV We. Tolle Wis--list SE ma Ilesdalar, thawPanded 1200030073. Pomade k w I s e CNJTION NM NO Mat an adt. AA100.0001m OM de Medd of MINN fawadi 30514 OWL Po lard wren daddy. Wadi *A oralWin memo padding set FlOt Netledlen Sudo 0113111 media *wad Bra albedo 1010470021. r101111111111111111111 AMUR 111.3014411.11000.DwAL CIIIIIIMMIIIM MI 12731 WIN 122.111 111111111140140 act WV Ma 1:4.211/305411M41$1.NOT S FEE OR L. 1111111~1111 sateediromang us 1111.71111111121.7 SNUG ISA NEIN CNIC 125.5 111111111113111mo VPII1mmlai No OWL 0. ismonommia nowru ow wrier de FIE moon 1131 111M00Oda 10 1113213*/ $120.071'11at 10. NOM PIE MOO. NV NM 130001002t. 1110/31 vowrompWNW bpi/ 15 MI Islow SOW Mt'. ole 211ON 1113014'11111111'05"N017' 5.4 NM lilt NS 101414111.1My 07. EOM NEW NOS AIVIII Wm. (1111111111111111111111 Onofeedody 1213 ad deftals at Wm.

MIIIIIIT Willi(130)7 w UTCr5(401)211'31'50.111132'2" 130$411111 100 O12 JACESMISUE 111111111111301110 mon um. MWM1111140101111". Dan. MO TM. Odd 270'. head. MIRKIIMIIIIMNININIEN043004 01011111111111111114$1111111 122.11 NOME (ONE LC 015.01111.110VM FILE GIL 111111IN 111A 1/L111122f OMME fie IMPORT WM ego) 11 It UTC41-401)2I25l53"$111'131rfl JAMMU IS 1 NIL 100. XT A. MOON UM CPRWu I) NW Iliali N110061300 %COMM 114114K 3400. NM V MK SWIM Niffl. NEL. fit ie. NEM NIFL OP WI MINN 1113000300 (AW 1105. 0200. 01400 HMI. IN St MN. ALMS. MI NEL WII(V414-11A 3.5' 7013V.TAM Odd 300'. Thew. NE We. Arresting dada. INN MIS Alwele 1200030011. ACTIVATEMIL lay 111.-30-123.0. 01111111111MOMMI11113AIM 127.71 11110111122.1 _ MS (MOO) LC MOON NOUN nu MOO. e mu 114.5(,137.47.')120.1(120',331') WON 120.15 ne. MU NM (10001004) NM 1111110111011 12115 mit 134.7 11/111111111111111101111 NOTAM RUE MOO. woe 0111Ple 1112 MCOChen MI 2132.33"N $1'20071' VI173' 5.7 NM to 30. 1110/1[. &Sam 5141/N 3111 I Mar Me (Is. PLYMOUTH)

NI Nerloge ad INIE..et am Melnelle weed dow.,Neld1W M Muer IWO wake adds saardiel mist 1M Mad are UTC adapt a Met

LEGEND 10.-Directory Legend (Semple).

13% Appendix 2

DMECTORY LEGEND LIMO This Maw is an elphisticel WWI of data an traced with the FM an all &Wore that ate open to the Public, modeled WNW cabal Willies, I mule traffic inlet centers and radio aide to nevigaden within the continence* United Metes, hole Rice and bee Iloilo Wends. Meets ate Wed elphabsticelh by awxisted dty nano and cross reformed by airport MOO Fecal* weedelel with an airport. but with a different news, we Wed individually under their own ewe, III wellin W ar the aiwtt with INN they are assedeled. The Using of an airport in VW direcbey ono* indicates the airport opetalor's Winans= to accommortele transient aircraft. and ems net twormint Met the twiny conforms with any Federal or local etendwds, Or that it has been approved for use on the pert of the general public. The inleilmliso on ektructiens is Wen from reports submitted to the FAA. It hat not been verified in aN cases. Plots ate arAsned Mat WWII met Mediated be this ebullition (or on cherts) tray (add which can creels a heed to figAt operation. WIWI "Wks conanimg antes and Mates tabu** within this direr:goy are contained Me Airman's Information Manuel, NW FN. Wansmtion and ATC Procedures. The hied Nees Pet fuses amok* be deli the cadent' of this Directory and an keyed to the circled numbers on the sample en Pe mewl% pew 0 cfromora not Aimee and WM* be this directory are lied elpfsbaticily by essodseed city and state. Where the dty name is different ken the Mnwt nee the city name WI appear on the line above the airport name. Airports with the same waisted city name WI be Wed arphelearialy by airport mime and WI be weraled by a dashed task line. AN others will be sweated bye solid rule Ant

0 NOTAN =VICE §--NOTMA 'If (Diana teletype disswinstion) and NOTAN V (local dissemination) service is provided for airport. Absence at anneletion i Mika* NOM 'V (lowl dissamineee , only is provided for airport. Airport NOTAM file identifier will be W ows as "PIOTMIFILEWY far M publicese Weeds. See AIM, beic Flight Wormstion and ATC Procedure for debited doselOws at NOTAM.

0 LOCATION REIMER A Wee or fes *wade cede wiped to airports. Thew identifiers we used by ATC Me New of the airport name Me Nighpiers, illgirt Wipe and Was WSW wads end compute' operations.

0 'sac LOCATION *pert es ten is wowed as diem and direction born the center of the associated city In nautical miss and cardinal wine, im. 4 NE.

0 TIME CONVENSION News e/ Illierallsn of all ladles we egresses! In Coordinated Universal The (UTC) and shown as r time. The directory Indicates Me war of hews te be subtracted from UTC to obtain load Warded time and local WOW caving None UTC-I(-40T). The we* 8 eddies tint during periods of DOW WO: tins effective hours will be one our odor than sheen. In these woes where des) ight swing tine is net observed that (-40T) and t will not be shown. AN setae deem daylieht wimp bus swept More and VW pow of Wiens In the Eastern Time Zone and Puerto Rice and the Wein islands.

0 QIOSWNIC Immo or Nam

0 CHANTS The UMW Chet and Lew and He Altitude Creole Chart and pens' an which the airport or facility is babel. *lees Chen *Mons MN be indicated la I.O., COYER.

0 11111111INENT APPROACH PROCEDURES PP MOWN an airport* which a presaited (Public Use) FM Instrument Apprised Procedure has been published.

0 LUNATION Dwation 1 Oven In fast above mean see beef and h the highest point on the lending surface. When elevation is seelevel it will be indicated ei (00). When Weston is below see lave a minus (-) sign will meads the figure.

0 NOTATING UNIT BEACON A Indicates misting Wean is'avoilable. Rotating beacons operate duet to dawn unless otherwise indicatedin AIRPORT WOWS. 0 somata $1:Mme, Wiliam 'spies. 112: SW SWIMS and mirror poworPlere repairs. EM:Meier airframe ard miner poweplent repairs. thl:Wier airframe and rater powerpInt WW2.

LEGEND 11.Directory Legend.

il'138 DIRECTORY LEGEND 0FM 0001 FUEL CODE FUEL SO leach S0 emelem pled) Jet 11-440e-cut turbine tun, 103 Orefle 100 patine (Omen) hems point-50' C. 1011 Made 10011. emerge Owe NM) (Slue) II+ Jet IIVAdecut babine lull with king inhibita, 115 Slide 115 gm** from point-50' C. A Jot AKweene *sue peint-40' C. AI Jet Sol Keresene, Imes point-50' C. Al + Jet 1,1-11ereearde ugh Mine Intabikr, Irmo pit -50' C. MOOS Atemmlik wens Mitch is le be used as alma* feel.

II T nil eMne Celia automobile wane may be used in specific aircraft alinesif a FM supplemental type has Men ebtelfwi Aulowable ovine which le to be used in *WAmines veal be identified N '11100Ar, howevor, the pale /type and ether octane nitre will not be published. Olio sewn an hod represents the most recent Infornition the publisher his been Mk to amino Beam= iveristy all faders, the fuel Weil may not okays be obleineMeby transient civil Mots. Conflenstion of aveilability et hal shall be amok directly with fuel dispensers at Motions where refueNniis penned. 0MIN OX 1 MO Pressen 05 2 Lew Resew, OX 3 Wipt PmesumMaimement SON OX 4 Lew PremmeItsplecannat balsa 1111101C MUNN RUSE Talk Palm Maas (T84The be tore shown is TPA aboveman ace level. The ascend epee in penniless is TPA Move almeit Is 40 moon esWIRY MID MOMS MOMS /WORTS fffNrpot a EabyA claw Almwt ef Entry Ware perneetion hem U.S. Customsis not required. however, at Mast one skew aloea anklet omit be leralshed. IONS AinsitftpicMisa pronlesion to land must be submitted la advance to U.S. Custom. At hostone affirt girememinelicoef what omit be Mobbed. !EEL maw mike of onkel at both an ACE and UM *pertmop be Included in the OW Men Oen filed M Conde er remark .This notice mU also be IMAM me an iiiase*-arUUL enema maimOMAN.amine may be reined Is Winn ONO Maim. Cemmllen. and U.S. Comermakallens %Mks by IIM4 pion.Use Want weft Is solely responsible kr boric Oa *mime million the asillitalls8 Oise Dilmee. Imadrallenand Nolurallestion. RMe NNW and ftricultunt Ommitimat repiremeek M the knomellomel FIME leformidien Menial for fieltwdank.) 0=IMAM /MORT WANno) Alp* amine Depsrlatmit erfrompoilelim 'Mad milers lid certified under FAR.Pan 139, an indicated by the CFR Wog I*, CFR Mks A. stitch rekleale the evekblity el crash, lire.Napa IIIMPINEIL FAR-PART 11CERTIFICATED I AIRPORTS INDIC13 MapANCRPIT FINE FOWING APO EQUIPMENT REQUIREMENTS lisquired Mport No. SdoduNd kik" *Win Alma* Larch Dap mess Hart+Wei for Ram

50080C or HAWN 1211 A 1 <90' 21 or 45080C + 100 p1 N=O 9 1 or 2 290', < 126' 25 India A + 1500 eel H20 I 2126',<159' < 5 C 2 or 3 2126',<159' 25 Index A + 3000 oaf NO 2159',<200' < 5 I 0 3 2169', < 200' 25 Wm A + 4000 EM IMO >200' <5 I E 3 _2200' 25 bidet A 4 6000 eel NO > Greekr Then; < Lees Then; a Equal or Onmiler Then; S Equal or Lam Than; DC-Ihy Chemical. /410-W4011

LEGEND 12.Directory Legend (Codes).

139 12 Appendix 2

DIRECTORY LEGEND The listing of ARFF hides does not necessarily assure coverage for nonair comer operations or at other than prescribed times for a'.: carrier ARFF index Ltd indicates ARFF coverage may or may not be available, for information contact airport manager prior to flight. 10FM INSPECTION All airports not inspected by FM will be identified by the note Not mop The Indicates that the aaport information hi,ran provided by the owner or operator of the field. 0RUNWAY DATA Runway information is shown on two lines That information common to the entire runway is shown un the first line while infomistin concernirg the runway ends an shown on the second or following line. Lengthy information will be placed in the Airport Mantle. Runway direction, surface, length, width, weight bearing capacity, lighting, gradient and appropriate remade are shown for each runway. Direction, length, width, lighting and remarks are shown for melon's The full dimensions of Weeds are shown, i.e., 50X150. WORMY WRFACE AND WWII Runway lengths prefixed by the letter "H" indicate that the runways are hard surfaced (concrete, asphalt) If the runway length is not prefbwd, the surface is sad, clay, etc The runway surface composition is indicated in parentheses after runway length as fellows: (AFSC)Aggrepte friction seal coat (GRVD)Grooved (TURF)Turf (ASPI) Pephaft (GRVL)Gravel, or cinders (TRTD)Treated (CONC)Concrete (PFC)Porous friction courses (WC)Wire combed (DIRT) Dirt (RFSC)Rubbented friction seal coat 1111111VAT MINT MAIMS CAPACITY Runway strength data shown in this publication is derived from available Information and is a realistic estimate of capability at an average level of activity. It is not intended sea maximum allowable weight or as an operating limitation. Many airport pavements are -wage of supporting limited operations with gross weights of 25.50% in emcees of the published figures. Pemessible operating weights, Insofar as runway streryihs are concerned, are a matter of agrewnent between the owner and user When &eking to operate into any airport at weghts in wens of those published in the publication, users should contact the airport menegement for permission. Add 000 to figure following S, 0, DT, DOT and MAX for gross weight capacity SRumay weight bearing capacity for aircraft with single- wheel type lending gear, (DC3). etc. DRunway weight bearing comity for aircraft with duel-wheel type landing gear, (DC), etc DT--Risrorg weight bearing capacity for aircraft with duel-tandem type landing gear, (707), etc DDT Runway weight baring capacity for aircraft with double dual- tandem type landing gear, (747), etc Quedricycle and duel-tandem are considered virtually equal for runway weight bearing consideration, as are smiletandem aril duel-wheel. Omission of weight bearing capacity indicates information unknown. RU MAT MINS Light we In operabon surest to sunrise. Wei n' available by prior arrangement only or operating part of the night only and/or pilot controlled and with specific operating horns are indicated under airport remarks. Since obstructions are usually lighted, obstruction lighting is not induded in this code. Unlighted obstructions on or surrounding an airport will be noted in airport remarks. Runway lights nonstandard (NSTD) are systems for which the light fixtures are not FM approved 1400 series: color, intensity, or spacing does not meet FM standards Nonstandard runway lights, VAN, or any other system not listed below will be shown in airport remelts. Temporary, ernwpncy or limited runway edp lighting such as flares, smudge pots, lanterns or portable runway lights will also be shown In airport remarks. Types of lighting are shown with the runway or runway end they serve. ?STDLight system fells to meet FM standards SALSShort Approach Lighting System URLLow Intensity Runway Lights SALSFShort Approach Lighting System with Sequenced NIM.PAndium Intensity Runway Lights Fleshing Lights HIRL-140 Intensity Runway Lights SSALSSimplified Short Approach Lighting System. Kit ftunwey End Identifier Lights SSALFSimplified Short Approach Lighting System with Se- CLce nterline Lights quenced Flashing Lights TDZTouchdown Zone Lights SSALRSimplified Short Approach Lighting System with ORALS -0' :red Directional Approach Lighting System Runway Alignment Indicator Lights AF OVRNAir Force Overrun 1000' Standard ALSAFligh Intensity Approach Lighting System with Se- Approach LOON System. quenced Flashing Lights 1.1)114LeedIn Lighting System. ALSF1High Intensity Approach Lighting System with Se- MALSMedium Intensity Approach Wrong System quenced Flashing Lights, Category I, Configuration MAL3FMedium Intensity Approach Lighting System with AL5F2High Intensity Approach Lighting System with Se- Sequenced Fleshing Lights. quenced Flashing Lights, Category II, Configuration. MALSRMedium Intensity Approach Lighting System with VASIVisual Approach Slope Indicator System Runway Algnment Indicator Lights

NOTE: Civil ALSF2 may be operated as SSALR during favorable weather condl'ions.

LEGEND 13,Directory Legend (Runway Data),

e ,

13 140 Appendix 2

DIRECTORY LEGEND VISUAL IIIINSLOK MOICATORS VAST Visimi Approach Mope Indicator SAVAMSimplifiod Abbrevated Visual Approach Slope indicator PAPIPrecisbn Approach Path Indicator P2I1 Zedmidai lied units placed on right side of runway Mit. 2- Identical lit units pieced on loft side ofrunway P4R 44denticst light units Moab on rioht skis of runway P4L Ngld wilts plaid on loft side of runway Sa 2-bou SAVASI on left eke of rummy $2R 24ss SAVASI on fight side of rummy V2R 2401VASI on right side of rummy V2L 2-boa VAS, on left site of runway V4R 4-bes VAST on right side of runway V41. 4-boo VAST on aft side of runway Vat ibat VASI en right aka of runway VEIL Ilace VAST on aft aids of runway V12 12-boo VAST on both skies of runny V16 1114a VAIl on both sides of rummy NSTO Nonstsidord YAM VAPI, marry sawsystem not listed above PAM/VASI awash slops or and threshold cromlng height will be shown when available;i.e.. GA 3.5 Tell 37'. PILOT CONTROL Of AIRPORT MINI. Mile Function 7 times withirWseconds Wise *malty avellabb S times within S seconds Medium or later intensity (Lower REIL or REIL-Off) 3 this within S stands Lowest intensity meibble (Lower Rat or REIL-Off) Available systems MN be indicated in the Airport Remarks.as follows: ACTIVATE PSALM Ray 7, HIRL Rwy 7-25-122.5. or ACTIVATE Mint Rosy 15-36-1223. or ACTIVATE VAN and REP, Rwy 7-122.11. Where the airport is not saved by an instrument approach procedure and/or has an independent emcification insbiled by the Wiped sponsor, descriptions type system of Afferent of the type lights, method of control, and opwating opleined in dear test the AK 'Rub Flied informetion frequency wit be and ATC Procedures.' for detailed descripdon of pilot WINN control of *pat WART MONO Runway pedant will be shown only when it is 03 percent or more. When availsba the direction of slopsupward will be maw, 0.5% Mr NW.

IMPRINT EMI MTA Lighting *balms such as VAN, MAWR, REL obstructions; displaced thresholds wit be shown on the specificrummy end. 'Mgt dc --4110-4 tunic indicates rift turns should be modeon lending and Wood for spaded rummy end. elmama mamma Landinglreo intlitelse Mnding chews for privet, or non-revenue producing aircraft In addition, teesmay be cherpd for pions the mein over a couple of hours and buyno services, or at motor airline tenths' for all Mae& s confinsd to operational items effecting the status and usabilitya the airport. M11311busimies.--SesPARACHUTE tabulation for detail.

2.4GEGaisnut0AdTleltDATA SOURCES Versother Guierving System

AMOS-I.reports *km* setting wind data and tow*temperature, dewpoint and amity altitude. AWC41.2nthsts the some as AWO1 plus visibility. AW063reports the some as MVO6.1 plus visibility andcloud/ viarq; lath See AIM, look Flight lidonnation and ATC Proceduresfor Mead dmaiption of 1W0S. SAVIRSIdsnlifies airports thet levee Sutplernental Aviation Weather Reputing Station *valetas to pilots for current cinatien. weather 111MLirnited Aviation Weedier Reporting Stationwhere observers mitt cloud height weather, wirriperstme end brepoint Gn most cowl surface obstructions to vision. wind, Member and Pertinent rernerke. U.WASIndicalm a Low Level Wind Sheer Alert Systemconsisting of a center field and several field perthwar TN .--Ilos RAINO NOS TO NAVIGATION anemometers.

LEGENL 14.Directory Legend (Visual Glideslope Indicator).

:141 14 Appendix 2

DIRECTORY LIQUID COMMUNICATIONI Csimunicalime WIbe bbd in sequence in the order shim ahem Common balk Aillwarg Frequency (CTAF), Adam* Tended Information Service (ATM and Abonadal Arkbory Stotler* MC P§ sag with their frequency Is shown, dere avelleble, en the line Mowing the heed% 'COMMUNICATIONS.' When the CTAF and UMW Is the sum frequenth, V frequency MI he dab as CTAF/UNICOM freq. Flpt books prom (Fie) IderneMlon. The modeled FES sill be ahem 'dewed by the Mandl* and Inhalation marling bellbillg of Wilms arab 4, Mod Lira (De). Leal Cad (LC364-2341). Legg Diana OD 2024261100 or LO 1402 51161212) elm TM Newt NOTAM M OM NI* MI be shown as *NOTAIA FILE YID.' Where the FEE Is haled on due field It M be 'noshed a be de Waft the lantifter. :mem des avelleble wM blew. The FES telephone number will follow droswIlk army.. _. eda* emeliond Infamistion. FM dime mime Is not the erne as the Nowt on which bated will also be Med in the idea elphibighth none bee for the ebb in each belled. Rennie Cermunkstiens Outlet (RCO) weaken make to Me sleet followed by the frequency end nom of the Controlling FES. FM's mobs lelemellue en almed oandldora, tadb aids end odor facildles, and process SW pens. Mart Messy Service Is "Mid au IM CTAF by FM haled at nonamiser drab sr eirperb who the lower Is not in speration. Ace MA. Poe 157/1511thaffic Arboary Practices d games saws a lower Is not in operelion or AC 90 420.) Aebtlrm ember IthslIrg sada Is podded Ig FES specideb. Fleht and bather briefing antes are else bobble by calling tebilbsei memliers het wyromed ak/ pound cmmunications facility. remotely caballed sod waken

sr deentwVie amide to Wendnoises the sonic* tenth of an FES. ammunketions frequencies used in the FES air/pound system are now operated Or"en TIIWIIMMIIMIL01V',&. 122.4. 122.6, 123.6; unerpncy 121.5; plus reatbonly on 122.05. 122.1. 122.15. and 123.6. a. LILO Is Meal is the Ennuis Fleht Wise bake channel at selected 133's. b.122.21 sniped ball Ms amenable weds shim swim c.123.6 Is sniped sew *pert advisory channel at rablowsr FES locations, Warw. It Is still in commission it some Flies odecoled wMA babe to amide part time Airport Wain Sankt d.122.1 Is Me Finlay mcolisthenly hiquency at VCR's. 122.05. 122.15 and 123.6 are amigned at selected VOW. model Mein whets. . Some FM ore meted SO idle chemists for dada amoeba in the 122.123 Pit bend (ep 122.35). blob using IM FIE A/4 system oho* refer to this d'ec'ry or speapriele deeds to determine frequencies salable at the FES or remeled bend Wm. did they wish b communicate. Part Me FES hems N walla are dawn in roads under Wily mane. Cwoograq frequency 121.5 Is ado* at all Flefit Seals badons. Toms. Appromh Control and RADAR facades, unless kilkolul se est evabble. Freepacies padded folleined by the leper T er gr. Indira that the fully MN only deem* or receive respectively on that beraway. Al rade ells to map** frequencies we transmit only.

CUPA peps. MOW to get all maths and aircraft d unowdreled airports on a women frequency. ATIEA anima beaked of baba rammed Inbred* in selected bees of Ngh activity. UNI00111A nenowinment ak/peund tale cormunkations faddy Wind to provide general airport advisory service. APP CON--Appood Creel. The symbol RP indkalse radar sperm* control. TOWERCoadel tower 0100011drawd Cored DEP CONOopedure Died. The symbol ei Indicates radar departure control. CLNC DELCluwance PRE TAXI CUICPre IM chorine* WR ADV611 SVCVFR Ad/eery baba Service prodded by NonRoder Approach Control. Wool thinks *VFW Atha (upon a wedded boob) de AM CON. AWN INC-11who Worry end Sequencing Service for VFR aircraft STACIE INCReahr Sequencing and Seperstbn Sento for peelcipethe VFR Alm-eft within a Terminal Radar Service Ares (TIS9) ARIA 'pert Roar bake Ara TCAIleder Ilardrare end Sepereden Servia for all aircraft Ina Terminal Control Arse (TCA) TOWER. APP CON and DEP CON MOW) CALI. Mil be the some as the aided nem unless Indicated °dyable.

LEGEND 1 5.Directory Legend (Communications).

142 15 ...... DIRECTORY LEGEND 0MOIOMOSIONAVIOAPON The Alpert Fealty Oirec lay Nets by tidily nom* all Neap Aids Is *Option,wept Military TACANS. the appear on National Omen Service Wiwi or Wft Aeronautical Charts and those upon which the FAAhas approved an Instrument Approach Procadurs. AMY,* VONTAC Ili and MLS equipment in the Notional Airspace Spam hasan automatic monitoring and shutdown beam In the owe of malhatelen. Umnordlored, as used in Vii publication forany noriptionel ! d, means that FSS or tower personnel area Name the malfunction or shutdown Orel. The NOM) NOTAM file identifier wigbe shown es 'NOTAM FILE IAD* and will he used en the Reda Aids to Nevigetion fine. When two or more NAVAJOSere listed and the NOTAM file Identifier is afferent then shown en Na Nada Aids Is Neapetion Nu, than it will be shown withthe NAVAJO leg% Hezerdous Mara Iffeeithe Aigiory Service (WNAS) will be shown where this Novice is broodiestover selected Wire. WAN) information is tabuisted as indicated in the following sample:

TWEE TACANANAE Channel Geographical Position Site Elevation 1 / riseversine 117.55 ME Chan 122(Y) 40'43'36''N 75'27'llrei HIV 4.1 NM to fid1110/81. NNW. 1 1 1 Claes FragrancyIdentifier / I Nearing and distance fibrotic VariationHazardous Might tality to airport Weather Afton Service

VOR unusable 020*-060 beyond 26 NM below 3500' / Restriction twain the normal altitude/range of the nerogsdonel aid (See primary alphabeticallisting for restrictions on VORTAC and voryoug. Nat Those ONE Wanner numbers with a (Y) suffix require TACAN Is beplaced in Na Y mode to receive distance Ilemitetion. MINSHrerane infftlit Walter Athisory Service la a continuous broodiest of infightwearier advisories including summaries/ MAUL cmwective SIGNIETs. AINMETs and agent PMEPs. HMS ispresently broadcast over selected VOR's and wiN be implansalat throuigaut the contenninous U.S. AllffilllIndicales thet SumMence (ASR) or Precision (PM) radar instrumentapproach minimums are published in U.S Govormaint instrument Approach Procedures.

MOM OM IIIMINATIONI

Mentillation of VON/YORTAC/TACAN Stations by Clogs (Operations) Limitations).

Normal Usable Altitudes and Radius Maw

Catena SIE Altitudes Zile Is (1) 12,000' and below 25 (L) Below 16.000' 40 (H) Now 111.000' 40 (H) Wean the Conterminous 4111Setes 100 only, between 14,500' and 17,999' (H) 16,000' P1. 450 130 (H) Above FL 450 100 (N) High(L) Low (T) Terming NOTE: An Off today is capable of moulding Q. and (T) service volumeend an (L) Willy additionally makes (t) service WNW

The term YON a operationelly, a were teem covering the IMF ormnidirectienal garbstype of facility without ruprd to the fact Na the pow, Na frequency probated service volume, the equipmentconflguretion, and operstional requimments may wry Whom fedillies at different Waft Al Aulwralie Walther Broadcast (oleo shown with I fahneng frequency.) OF Iffrection Finding Suva. OK UHF standard ( TACAN compalMe) distance mourns squawk ME(Y) UHF termed (TACAN compatible) Selena newel% equIprient that requireTACAN to be paced in the '1" mode ti rash, ONE. H Noodirectiensi rase bacon (lamina power 50 watts to less then 2.000 watts (50NM at all altitudes). NH Nonairmeenel radio bacon (homing), power 2,000 watts ormore (75 NM at Si altitudes). MAO Nonairectienel rale bacons provides automatic transcribed wasther elate. NS inetnenent Landirg Salem (voice, where available, on exam cannel). IIMLS intalm Standard Microwave Landing System. LOA Locailar Diredlond Aid.

LEGEND 16.Directory Legend (Radio Aids toNavigation).

143 16 Appendix 2

DIRECTORY Ulkl Cowes loaner Mann Own installed at wink minter site (15 NM at MI anAwdes). LOU Canyon looter Oben Own Mann at haw wader site (15 NM at aN altitudes). MN Nodirectionel radio noon (honing) power Ins then 50 watts (25 NM at MI altitudes). AS Mamma lain% !)alma II Simultennus ramp homing al/rat end/or voice Val Naniiroctienol radio Neon not authorised for Wit or ATC. Provides automatic weather breoloste. KIF lit. oilled Nadia Fanny. TANN UHF navIgelleral lainlywrin ..1d1r..s.-Al aurae and distance informetion VON VHF menpllanal foci itywnininectionol course only. voaiome Collsoled VON minion' faclay and UHF standard distance meowing equipmwt. VONTAC COMO VON and TACAN nevletionel facilities W WINO nice in oft NINO froinincy. 2 VIW steno nation mono at a li radio facility.

FREQUENCY MINS FUN AND INS CNANNEUNG as VW TWIN 1115 NIF TACO NO Mhr NMI NNW mow COMO COMM maw CNN CONN engem OWN KO 10110 182 Sill 109.45 31Y 634 114.03 $7Y 502 106.30 202 570 109.56 32Y 636 114.15 NY IN 108.50 22X 572 105.65 33Y 638 114.25 NY 506 10170 242 574 109.73 341 NO 114.35 90Y 505 10190 252 576 109.65 33Y 642 114.45 91Y 510 105.10 262 576 109.95 36Y 644 114.55 92Y 512 109.30 3N 580 110.03 37Y 646 114.65 fOY 514 109.50 322 562 110.15 31Y 648 114.75 94Y 516 109.70 342 564 110.25 35Y 650 114.65 95Y 518 100.90 362 586 110.35 41f 652 114.95 NY 520 110.10 38X 5N 110.45 41Y 654 115.05 97Y 522 110.30 402 390 110.55 42Y 656 115.15 9SY 524 110.50 422 .42 11015 43T 658 115.25 99Y 526 1/0.70 442 594 110.75 44Y 660 115.35 100Y 528 110.10 462 596 110.85 45Y 662 115.45 101Y 530 111.10 411 595 110.95 46Y 664 115.55 102Y 532 111.30 502 600 111.05 47Y 666 115.66 103Y 534 111.50 32)( 602 111.15 NY 618 115.73 104Y 536 111.70 542 604 111.25 49T 670 11515 105Y 538 11110 562 WO 111.35 SOY 672 115.95 101? 540 1011.05 17Y 608 111.45 51Y 674 116.06 NOV 542 106.15 lrf 610 111.55 52Y 676 116.15 108Y 544 108.25 19Y 612 111.65 SOY 678 116.25 109Y 5411 108.35 20Y 614 111.75 54Y 6110 116.35 110, 548 108.45 21Y 616 111.65 55? 1182 116.45 111Y NO 10156 22Y 618 111 95 56T NM 116.55 112Y 552 105.65 23Y 620 113.35 SOY 686 116 65 113Y 584 106.73 24Y 622 113.45 NY 6118 116.75 114Y 556 101145 23y 624 113.55 82Y 690 116.85 115Y 585 10195 26Y 626 113.65 03Y 692 116.95 llrf NO 1011.05 27Y 628 113.75 84Y 694 11706 117Y 562 109.15 25Y 630 113.85 NY 596 117.15 1111Y 564 109.25 29Y 632 113.95 NY 695 117.25 119Y IN 106.36 NY

LEGEND 17.-Directory Legend (Frequency Pairing Plan and MLS Channeling).

144 17 ENROUTE LOW ALTITUDE-U. S. LEGEND AIRPORTS Airports/Seaplane bases shown m SLUE have an approved Low Ahrtude Instrument Approech Precedwe publnhed Those shown o DARK BLUE how on approved DOD Low Allow', Monument Approach Procedureand/or 000 RADAR MINIMA publehed m DOD PUPS, Alaska Supplement or Alaska Terminal Awports/Seeplone bows shownin MOWN do not hove a published Instrument Approach Procedime Published 11.5 and/er locolices !YIN Landing Cpabil Mena indicates LAND SEA Welee on regent or operetiogg:etriid Procedure available night only Code Indio:Om Pilot Go Gel Published SDF lighting (Pa). For Information mime 0 Procedure available Directory or NM IR Swpfornent oo biro Civil-MR*0m IParenthews wound carport name Weary indium misery lending rights not Rader Services 00 Illyieport Elevelion tallebwp Haw, evadable ®® 2 Airport Notationgiveninfeet above or below noon sea level RELATED PAOUT1ES 3 length of longest runway gwen to **; 34r Poe to Metro Service (PMSV) nearest 100 feet wile 10 feet as the s--',Ans*los.s f Longest Wean@ 4141/ Cootinueut OAHollon Minding pant (Add 00) Aimee* TennInal e.sy with 4 Airport symbol may be offset kw Information Service ow end Frequeray_i LWthen Continuous *movie noweahon auk S Pvt - Anew use, not available to Slot undoes.; general public opmahon less than O Weather Rader (WXR) connuousti or 6 A bet encloungthe wiped name pert haw indicates FAR 93 *wool Require- PMSV end VAR Combined No R Insketes ments - See Directory/Supplement lighting la=elly Soft Swims RADIO AIDS TO NAVIGATION ANDCaftiffie2tfism RADIO AIDS TO NAVIGATION RADIO MOS TO NAVIGATION AIR/GROUND COMMUNICATION 1/14F/UHF Data is depicted on MO DATA BOXES IF/MP Dan is deptcted in BROWN SORES HEAVY LINE SORES ladicate Flight Service Stations (FSS). Frequendes 2534. 122.2. COMPASS ROSE Abnormal Status Underpnnt for effected Oriented to dote,g . SHUT DOWN, and einem. 243.0 and 121.5 me Rem* megnitto north Sae MAY SE COMSN. etc available at ell FSS's end me net shown of compost row has Me.. bones All other fiespreedes no signshconce. available at FSS's am shewn. Sivalm sins ore Frequencies mem* and realty mcept thew followed by R or Ti R - make only used in congested I - tronenit °my 0111011. ONE MHO DOWN 123.6 122.6 122.1 R NAME 0 V' NAM rri. 000,1(7) VON TACAN VOYAC DALE Ow IS MN = r 000 Airport Advaery Smoke a VOR won TACAN compatible D1-7 (AAS) 123 6 ND./ONE A sold square indicates information wad- Frequencos petitioned above Min tine able Ewante weather, when available, is NAVAID boxes mte maned Is Me NAVAID eht 19/14F Nondiremotnel Rodiobeecon-broadcasted on Ow emaciated NAVAID r;or Menne nockobeacen with Other frequenaes of the controlling FSS frequency For terminal weather frequencies morale north indicator ' we A/0 Frequency Tab under associated named are mailable, hemmer. altitude and airport twain may detertniee their recoption Name end UHF Non-Machonal Itadiebeecon rn Frequency protection FAYETTEVILLE FYVidentifier for Usable range at 12,000' - 25 NM FSS net amodesed with goComp.. Locator Beacon 122.1R NAVAID TACAN st be placed in "Y" Centel°, Station lT,/ mode to receive distance Rif orrnoken Ground Control Intercept (GO) ConHoltleg FSS Operates less NAME than continuous OfOn Request NAM:-L This brie boo, without frequencies and controlling FSS name indicate' an FSS DME Chen 00\ frequencies available NOB with DME 0 Flight Service Mahon (955) --11=1 Remote Communications Oullet (NCO) RS lecoloor Count wile ATC function Underline indicates No Voice Feathered ode indicates Slut Sector Transmitted on this frequency TACAN channels ore with CTA/ FIR voice but are not underlined EMES NAME Typo of onto traffic now SDF Lowliest Coon* with ATC function U S Weather Station FL 18 adie-with Voice Minkel limits of costae, Communication GND CON IDE N T 0 corn mita& A/0 Voice call and 000 120.5 frequency Broadcast Station ACC Unit providing ATI

LEGEND 18.En Ftnute Low Altitude- U.S.

145 18 Appendix 2

For use op to not i lisp 18,000' MSL

AIR TRAFFIC SERVICES AND AIRSPACE INFORMATION AIR TRAFfC SERVICE Omll Wimp (Right BOUNDARIES ROUTE DATA Ilionning end Mildew Altimeter Setting Change IFN Neuter) 1/14F/LRM Done 11 Melded in BLUE eh (A) ehMinister Setting Change Ul/tAP Does Is depigml le BROWN when not °Minns. defined X Mileage Breakdown I Air Route Traffic Control VON Airway end 42 Center (AMC) Noreilleollon VOR Changeover Point NAME ARTCC Remand Sites with LF/MP Airway and 11**8 **IMF * Name discrete VHF and UHF Aids (Net shown at 134 3 2695 frequencies idesolloodoo msd-peint locations) UncomrellW Oceanic Control Ana (CTA)/ =inett. TACAN Ti Dole Flight Information Region (FIR) Chan hisr Air Defense Identification Ram anal Zone IADIZ) imessioeo I SO' /5 Dinner hem TACAN hem TACAN Combined ADIZ and FIR Inlowne Ram end Oceanic Control Wenlawden KVEN Direction of Flight Control Zone (effective 24 Atlantic Neale and Indicator (Concha only) hours unless otherwise idoneMmelon Minimum Ennwh nand) ..GMBED. Om* Ram end Altitude (MIA) 6. Canadian Class" C" Control identikatien Ahnonwin Oben/Wan Zone Clearance Altitude errsroes Wes Canadian Aerodrome Traffic (MOCA) Zone 19106Rose 1 1411NR9 Mosimum Authorised NIAA 1 3500Altitude (MAA) Control Zones within which 4:11-0-0.00-0 Soltellosee Rouse iTTTThaecwing special WI flight ME& MM and/or is prohibited Use Nelms se Arywoories public/hen MOCA change of other for walk Inhovemlo -I then Rodin Aids mumNon-Free Flying Am* (teeth nsigtion pant to area) AAA,UninoNo or Closed WigSuffer Zane (teeth point Segment Mumma Recephon MIMI' (MIA) to area) 1110, 7:Owed Singh Internationol lioundary DIroMoo Abney Crossing Ahnirde (MCA) (matted when coincident with Denotes DME fix (distance Shaded area (brown) indicants uncontrolled sewn ac noway whop) airspace Damp botereon vIver In Alaska - indicates 23 MVOs, Rothe Denotes WE fix (encircled designated controlled RA.Witai/et Mame EL"Weep sheen when not airspace outside the 23 Bresielmen otherwise obvious) continental control area above 14,500' MAMIE OfGROUPING In Conado - indicates designated controlled ektreplkM4411.4 airspace above 12,500' tillik:Ortsam) MISCELLANEOUS .---- 1985 Isogonic Lone tom61 IWO and Value

ALL MILEAGES Al! NAUTICAL EXCEPT AS NOTED ALL RADIALS AND BEARINGS ARE MAGNETIC ALL ALTITUDES ARE MSL UNLESS OTHERWISE STATED AU TIME IS COORDINATED UNIVERSAL (STANDARD) TIME (UTC) SOURING PERIODS OF DAYLIGHT SAVING TIME (DT) EFFECTIVE HOURS ire WILL II ONE HOUR EARLIER THAN SHOWN. AU STATES OBSERVE DT EXCEPT ARIZONA AND THAT PORTION OF INDIANA IN THE

LEGEND 19.Air Traffic Services and Airspace Information.

19 146

111101111.1.11.4.1. Appendix 2

HELICOPTER ROUTE CHART NEW YORK LEGEND Consult Anport/Faality Directory (A/FD) for detoik involving airport lighting, navigation aids. and unit.. AIRPORTS AIRPORT DATA Indicates Flight Sonia LANDPLANES FSSe Station on field. Hard - surfaced runways 1500 ft or greeter Boo ondicatos Spool :Mit'14 CT -110.3* Traffic Ants (Us FAR3) ATM 124.1 Al rscognaeble hardsurfaced runways, intim:long those * 03 L 122.55 UNCOM closed. ore shown for moral Identification Unverified Heliport --....(Unverified) 0 Other than hardsurfocod public use Airport of entry FSS - Night Sonia Station 'mate use CT - 114.3- Cant* Tower (CT) - Co) primaryfrequency * - Sew Vurvektv itelinetion eon Woe See tower frequencies HELIPORTS OTHER tabulation for beers at operation Ans124.5- 0 andliefipopubic 0 Ultrolght Flight Automatic Terminal laforrouttion Sonia ndinrhnate Park Soloctod UNICOM - earenavticel whomMelon 03 -Elevation in feet Hotpital Seaplanelose L - lighting In operetion Sunset to Sunrise 0holmods L -Witting avoiloble on request. parfrnme lighting. or Trauma plot-controlled 1111/Center When facility or infonnation is kicking. the rospactim decanter Holipads located n replacedby doh Al lielolne cede. refer te noway Id". lbwat motor airports All *nos two loco!. NECT - Nee Federal Ontfrol Tower * Rotating light on operation Sane to Sams. RADIO AIDS TO NAVIGATION AND COMMUNICATION BOXES VHF OMNI RANGE (VOR) 122.18 122.11231 raw lino boa sndicotss Fight Simms VORTAC OAKDALE %Men (F55) From 121.5 172.2. 243 0 I3112 1111.11 OAK Dr' and 255.4 as. Newell" evoiloble at MI 0 VORDME FS.Ss and ore -shown abovebens. 122.1R Al ollwor freq. ... thews. Undertoneondsc2 NOnatrechonal For Almon Mammy Semite no moat on this hal 1E2=1 ow FSS keg 12716' E.' Radoobeocon R - mono only In Canada ell available FSS frequencies are shown -ssFrequoncios above thin line boo Sr. twinned Other facilites, s e , COMMIKIA MIAMI to NAVAJO use. Other frogs at controlling O Broadcast Stations, FSS Outlets Conttothng F SS FSS may be wobble detanvonal by altitmla RCO. Mc and terrain Consult Aleport/Fedlity Moder/ for contpleto information AIRPORT TRAFFIC SERVICE AND AIRSPACE INFORMATION Only she controlled and served compare offochvo belowHomoIt M5l are shown en Est chart Al times aro local. HELICOPTER ROUTES PRIMARY I: WI SECONDARY Rout. Tower Arrow indicates AINNda Importing Nome Frequency One way Route ChongtonwHolding Point OR MILITARY Point TRANSITION io4 do* A1.40^-C10Pvilvv/ 500 Maximum Route Altitude ComPitivvY

ALL ROUTES ARE RECOMMENDED ROUTES ICThmilmiP11011 RIME WHEN AuniONIZED TO OPERA THE TO, INDICATED, ALTITUDES WILL RE ASST TILAPPIC CONTROL. HELICOPTER ROUTE AL NpT RELIEVE PROTE-FROM THEIR DUTY T 1311203 PROPS ARE WE= TO FOR

LEGEND 20.Helicopter Route Chart.

147 20 Appendix 2

AIRSPACE INFORMATION OBSTRUCTIONS TOPOGRAPHIC INFORMATION 1000 ft and Ascher AGL Xis - Tentoinol Roods Gwent Area 300 ft and higher AGL A Railroad

TCA Surface Power Arta Tranunnsion or/A cffeuobz. Lone

Obstruchen with Catenary Hoght ARSA - Airport &Intensity hgMs greater than 200 ft. Roder Serino LI May operate port time Area 2049.- Elevahon of the top andges and Special Airport 149) above mean sea level Viaducts Traffic Areas UC hescht above ground 7iP -',Under construction or Special Air Traffic Rules reported: passion and O Race Track on P.A.R. Part fa for details) thevation unverified Tankwater, Prohibited, Restricted, CAUTION. Guy wires may oil or gas **** Wong% end Alert Area extend outward ham structures yt Mows And At0A ?Wary Quarries Operations Anto MISCELLANEOUS IF Outdoor Gads. Uhrolpht Theater - Military %Wog Bute Athvoty fx - Combat Zone a- Emends upwards c9 horn the surface CZ within which TTT fuel vii special WI TI MIS NECK MOSE Plight is prohibited IMO mu On Clots C CZ (Canada) Pictorial Symbol gstsParachute Jumping Area y Sae Aimed/Peolny Directory

TERMINAL CONTROL AREA ALTITUDES

70--Ceiling of TCA in hundreds of feet MM. +10- -Floor of TCA in hundreds of feet MSI.

(Floors extending "upward from above" a certain altitude are preceded by a + Operation at and below these altitudes are outside of TCA)

ATTENTION THIS CHART CONTAINS MAXIMUM ELEVATION FIGURES (MEF) The Maximum Elevation Figures shown in quadrangles bounded by ticked lines of latitude and longitude are represented in THOUSANDS and HUNDREDS of feet above mean sea level The MEF ms based an information available concerning thehighest known feature in each quadrangle, including terrain and obstructions (trees, towers,antennas, etc )

Example. 12,500 feet .. 1 25

NOTICE TO USERS OF THIS CHART You are urgently requested to Inform us of corrections and additions that COM to your Montan while using this chart Postagepaid Chad Correction cards are available at authorized chart sales agents and at FAA Flight Service Stations. Where delineation of data is required, such information Mould be indicated clearly and accurately on a current chart (a replacement copy will be returned). Mail to National Ocean Service, NOM, N/CG31, 6010 Executive Blvd., Rockville, MD 20852 or call toll-free 800-626-3677.

LEGEND 21.Helicopter Route Chart.

148 21 Appendix 2 ------L-1Amoati Airports shown have a minimumof 5000' hard surfocred runway.Airports in SLUE and GREEN have an approvedInstrument Approach Procedurepublished. The DOD PUP Terminal High Altitude containsonly thou Acorn in RUE .. <> 6 toe'd . . Mint ChilWAIlhoty1 macePostvitio.y4141441640.4410011,07044 kwAhlorlaweiseiffievimr490.0441,he dill441iideIII1 0 0 0 "aisrl net erssellobee RADIO AIDS TO NAVIGATION NAVAIDS IDENTIFICATION SORES VFIF/UPW Mk andepicted in MACK -Me If/MP A.I. ore dimmed in MOWN NAMEmity) / h- NAME (000.0 7,4 C100.0 NAIE(L) 00 COMPASS ROMS neemaer Oriented to POCK PICRAMS Mere* North OnwprMt el Oases/ Shentow ha Mahlon FSS and of NAVAID which Mao indlosees Mmwmal rose old mom nom may not be Stowe mihnse4 so the (PSS heels twelableme255.4 122 2, dialed minipanic (Y) Wholes '11. mode regoined lot romptien Wetted dumb frogs and men 213.0 solves amel 121.5)

LF/MF NAVAIOTilv'SS"1".haeTTal"." 100VHF alkssas 11.44 ___,,h14^.64.4",______In Cowls 'Modemhen Meanies i di 1 1 "n" "'"1.'"V *Mom wills demistel pimp hog 243.0, VOR VOR/01/3 TACAN VORTAC 121.7 or/ 121.5 trfine Nenilirectionel (t) ftegesoce Preteclen %Maerentsat Indieboomin so Marine undercut indiums Ns Voice en OM 11.000. "0 TOT. *L. TTorrt. ,Ndlit a* inelloboscon frounency. TACAN Chamets ere without Vela bus me :es underlined w"*""led11"*.1" "" UHT hiessillrectlenol (T) hespionq Proem:11m ...... Usable rants ad eedlebermen 12.000` - 25 NM. 'r located Of let ream :rei=maildli: Pa LIVMF NwHrecosnol mes WO aMobncon/ON3 left Aido Noigstn widn* Classillootion on If CMINITIV

MCC three letter idiots and HAEFAS frequencies, Albuquerque ZAS (127425),Atlanta M, Boston Mi. Chicago ZAU, Cleveland ZOS. Denver ZDV (135.525), Fort Worth IFW, HoustonZHU (126325), Indlonapslls ZIO, JocksonviNe LOC, Kansas City ZKC (126.475). Los Angeles VA (ISSN). Memphis VAE(133475). Miami ZMA (132.725), Mneopolis ZMP, New York (ZNY). Oakland ZOA (135.7), Salt Lake Cis),ZLC(133.025). Sande ZSE (135.925). Washington ZDC P-PROHINTED, R-RESTRICTED, W-WARNINO AREAS CANADA: CYA-ALERT, CYD-DANGER, CYR-RESTRICTED AREAS All altitudes are MSL unless otherwise indicated Time - Hours shown ore UTC unless oiherwiee Days - Sunnse to Sunset exams Canoda where indicated it means 14 hr before sunrise to h hr Continuous -24 hisday and/er 7 days a week after sunset MonFri - Indkates that area Is active every day Nights - Sunset to Sunrise except Canada where from MonJay through Friday it means14 after sunset to IS hr FL - Flight Level before sunrise ; During periods of Daylight Saving Time (01) effer ties hours will be one hour earlier than shown

I EXAMPLE OF GROUPING Iffiectim Those of Single Direcaor &who ti,7ke Newt* comeeNne bymmeing a today which n ran pan el this specific mute r- Hoak* Poem KARCY I CD _091 /11 ir.... 271 117®MEA3 000 1 10 117 AMM.Or~warJIII Salected Waling nsperting points hove amerdinete winos shown

LEGEND22.Airports.

14922 9A II 1 II I lip 8 8 H$ 11 illi7 I I I Iliri II II d1 x171 ii iilitli9iPpit tiff itiii alirrtli5 Zrn 11/11-1% g Igorrttif I 11Y ° c -etmi -4 Ulligni 1 i> t> . MilI to+. 81-18 m ni5/7,11P it> 'itt 1 1 11111111 PPP i1! p FP iiiqui = ° : r i If i wit PTPIP" 11 ifll to iiiiifttI 1 Iitltitti iI111111!P1 itr fl It , _ 1 =IC 11!11 ig t 0 1111iltri ili a Ifif 1 1 M di V,. i ;WillIii 11}1 A. I "9 g rf3,1, I 4101 itfMI i 1 lif iirft iRIP ii 1 c li Iiiil mit! of 1 fiea1.1ifii i 11iOh in I gil11 I I41 1 2 LI§ PI .4, II , f172.1C IM Aerials Table

( II 112) (31 (4) (A) 171 Maximum met quantity riockagmig Water %Moment. en ose package i Label(s) Vii Hazardoss materials dose dolmas Hazard required (a) (b) I a 1 (b1 ( a) MI )c1 sad proper shapable sautes et as A 114 not Paaenger Specific excepted) Carrying Cargo c Fa.. Eaceptioss require. only 'weer aircraft vemel Other requirement. meets or railcar aircraft vessel m Accuandalor. preemsrised (pneumatic or NO111481111111111. Nosflastma 173 306 No Mist No lung 11 1.2 Sydrastic I, comemesei osiglamsmattle gas Me gas Ms gas Agetal Flammable Fissionable 173 11a 173 119 I quart )0 galleons 1.3 liquid liquid Acetaldehyde (ethyl aiirarde 1 Flammable Flammable None 173 119 Forbid- In gallon% 1,3 liquid liquid den A Acetaldehyde mamma ORM-A Nome 173 505 173 510 No limit Ni' limit ArIIC acid (44erusts solitome) Corrosive corrosive 173344 173 245 1 quart In gallon. 1.2 1.2 Stow separate (runt nom ad or "ludo material mg materials Acetic acid. glacial Corrosive Corrosive 173 244 171 241 I quart Iii gallon. 1.2 1.2 Stow separate from nom at w1 or no du material mg tualenal5 Segtegalson sane as I.' flammable liquids Acetic ashydnde Crimson C wive 173 244 171 24i 1 quart 1 gallon 1.2 1.2 mate nil Acetonic Par ,r she Flammable 173 114 171 119 I gaol 10 galkins1.3 Isquto liquid Acetone cyanohydnn Poona II Poison None 173 144 Forbid- it ga11005 1 5 Shade Dom radiant heatStow w+., den from .orrouve materials Ammo oil Flammable Flammable 173 II It 173 119 I quart i o gallons 1.2 liquid liquid Acetnarlode Flammable Flammable .73 I IS 173 119 I quart 10 gallon. I a Shade from radiant heat liquid liquid Acetebesanyt peroxide, solid Forbidden Acetyl bessoyl peroxide solutes, ono Organic Organic None 173 2 ,. 2 Forbid- 1 quart 1.2 ewer 40% "mob peroxide pommels den Aa7tyl bromide gas Corms. ,oe Corrosive 173 244 173 247 I quart I gallon I I Keep dry (.lass .arhoy4 not permittet material on passenger swan).

LEGEND 24.Hazardous Materials Table (CFR 49 Part 172). ,e,

1172.101 Hazardous Materials Table ( cont'd ) 0

111 121 131 141 151 161 171 Maximum net quantity Packaging Water shipments tonne package , Label(%) la i 1b1 111,/ Hazardous materials des.zriptions Hazard requited (a I 1 h 1 la I (h1 (Cl and proper shipping names clam 1 if not A Passenger Specific incepted) carrying Cargo Exceptions require aircraft only 11 sense, Oraer requirements mints or railcar aircraft ("4 vessel ..... Acetyl chloride Flammable Flammable 1 /3 244 171 247 I quart I gallon I lucid I Stow away from akohols Keep smo1 kind and dry Separate krapturanally by an intervening titmplete compartment or hold from exranutes Acetylene Flammable Flammable None 171 301 Forbid- 1rat I 1 Shade from radiant heat 1110 gas den pounds AAcetylene trarabromide OR MA None 173 505 173 510 10 gallons55 ga!lons Acetyl radicle Corrosive Corrosive 173 244 171 247 1 quart I gallon I I Keep dry Glass carboys not permitted material on passenger watts Acetyl peroxide solution. not over 21% Organic Organic 171 151 171 222 Found- I quart 1.2 crennwle perms& perorade den Acid bray{ phosphate Corrosive Courant 173 244 173 745 1 quart S gallons 1.2 1.2 Glen craftily. in hampers not permitted material under deck Acid carboy empty See Carboy. empty Acid, brand. n o s Cortrative Corrosive 173 744 173 2... 1 quart I pints 1 4 Keep cool material Acid. sludge Corrosive Corrosive NOI4 171 2411 Forbid- 1 quart 1.2 2, material den Acrolein. Inhibited Flammable Flammable None 173 122 Forbid- 1 quart 1.2 S Keep cool Stow away from living quar brand liquid and den ten Poison

Acrylic acid Corrosive Conceive 171 244 1 173 245 1 quart S punts material a Acryloratnle Flammable Flammable None 173 119 Forbid. I quart 1.2 S Keep cool 2 liquid liquid and den Prawn

LEGEND 25.Hazardous Materials Table (CFR 49 Part 172) (Cont'd).

153 154 1172.101 Hazardous Materials Table (cont'd )

111 12 13) 14) 151 161 17) Maximum netmama, Packaging Water shipments in one package ei Leask.) le) W/ Ma'am. mom& deacriptscm !bawd required la) (b la) lb) la) lb) A sad proper skipping sasses claw Moot Parma elicPlad) SFcific carryiag CargoPas- Cur Other requiremeas Except require' aircraft "IY valid"et manta or raik:ar aircraft vowel

Allivl Manssnam halide: See Pyrnphorsc limo& a o s AAllethrin ORMA None 173 505 177 I No mit No limn Ally1 alcohol Flammable Flammable 171 118 17, 151 1 quan 10 gallons 1.2 liquid liquid and Poison Ally1 bromide Flammable FlammaMe 173 11X 173 119 Forbid- 10 gallons 1.2 liquid liquid den Ally! chloride Flammable Flammable None 173 119 Forbid- to sadons 1.3 Ivied Mood den Allylehlorocarbortate "-tamable Flammable None 173 2XX Forlud- 5 pow I 5 Keep dry Separate longsurhaalfy by an liquid liquid den saterwaing complete bold or wman- men* Nom explosives Segregation same as for corrosive materials Allyl chloroformate See Allyl ckInvocarbonate Allyl trahloroalane Corrosive Corrosive None 173 211 Forbad- 10 gallons I I Keep dry material den Aluminum alkyls See Pyroplsnrsc lulus& so. Aluminum Mumstle. anhydrous Corrosive Corrosive 173 244 17324Sb 25 100 1.2 1.2 Keep dry 110111fila I pounds pomade Ahmanson dross, wet it hot See Sec 173 173 Segregation same as for flammable label Aluminum hydride Flammable Flsaisiable None 173 206 Forbid. 25 1.2 5 solid solid sad des pounds labeled Dangemus When Wet Dangerotra whoa wit

LEGEND 26.Hazardous Materials Table (CFR 49 Part 172) (Cont'd). 155

1 :5 Appendix 2

EXCERPT FROM CFR 49 PART175

PART 175CARRIAN BY AIRCRAFT

Subpart A--Clortorel infornation and Regulations Sec. 175.1 Purpose and scope. 175.3 Unacceptable hazardousmaterials shipments. 175.5Applicability. 175.10 Exceptions. 175.20 Compliance. 175.30 Accepting shipments. 175.33Notification of pilot-in-command. 175.35 Shipping papers aboard aircraft. 175.40 Keeping and replacement oflabels. 175.45 Reporting hazardous materials dents. Subpart I--toedine, Unloads. and Noodling 175.75 Quantitylimitations aboardair- craft. 175.75 Storage compatibility ofcargo. 175.79 Orientation of cargo. 175.85 Cargo location. 175.90 Damaged shipments. Subpart C--Sposifk Regulations Applicable Accord*, N Classification of Material 175.305 Self-propelled vehicles. 175.310 Transportation of flammable liquid fuel in small, passenger-carrying aircraft. 175.320 Cargo-only aircraft; onlymeans of transportation. 175.630 Special requirements forpoisons.

LEGEND 27.Excerpt from CFR 49 Part 175.

157 27

NIMINI.A.1.--.....-.-.---,--- EXCERPT FROM CFR 49 PART 175 I 175.1 Title 49Transportation Sec. (2) Aircraft parts, equipment, and 175.040 Special requirements for otherreg-supplies (other than fuel) carried by ulated materials. an aircraft operator if authorized or 175.700 Special requirements for radioac-required aboard his aircraft for their tive materials. operation including: 175.710 Specialrequirements forfissile (i) Fire extinguishers; Class III radioactive materials. (ii) Cylinders containing compressed Mr:marry: 49 U.S.C. 1803. 1804. 1808: 49gases: CFR 1.63(e), unless otherwise noted. (lit) Aerosol dispensers; Souses: Arndt. 175-1, 41 FR 10100, Apr. (iv) Distilled spirits; 15. 1970, unless otherwise noted. (v) Hydraulic accumulators; Non: Nomenclature changes to Put 175 (vi) Non-spillable batteries: appear at 43 FR 48845, Oct. 19. 1978 (Arndt. (vii) First-aid kits; 175 -6). (viii) Signaling devices; (ix) Tires; and Subpart AGeneral Information and (x) Items of replacement therefor. except that batteries, aerosol dispens- Regulations ers, and signaling devices must be packed in strong outside containers, ; 175.1Purpose and 'type. and tires must be deflated to a pres- This part prescribes requirements, insure not greater than 100 ps.i.g. addition to those contained in Parts (3) Hazardous materials loaded and 171, 172 and 173 of this subchapter, tocarried in hoppers or tanks of aircraft be observed by aircraft operators withcertificated for use in aerial seeding, respect to the transportation of haz-dusting, spraying, fertilizing, crop im- ardous materials aboard (including at-provement, or pest control, to be dis- tached to or suspended from) civil air-pensed during such an operation. craft. (4) Medicinal and toilet articles carried by a crewmember or passenger in 1175.3 Unacceptable hazardous materialshis baggage (including carry-on bag- shipments. gage) when: A shipment of hazardous materials (i) The total capacity of all the con- that is not prepared for shipment intainers used by a crewmember or pas- accordance with Parts 172 and 173 ofsenger does not exceed 75 ounces (net this subchapter may not be acceptedweight ounces and fluid ounces); fortransportationortransported (ii) The capacity of each container aboard an aircraft. other than an aerosol container does not exceed 16 fluid ounces or 1 pound ; 175.5Applicability. of material. This part contains regulationsper- (5) Small-arms ammunition for pertaining to the acceptance of hazardoussonal use carried by a crewmember or materials for transportation, and thepassenger in his baggage (excluding loading and transportation of hazard-carry-on baggage) if securely packed ous materials. in any civil aircraft inin fiber, wood, or metal boxes. the United States and in civil aircraft (6) Prior to May 3, 1981. radioactive of United States registry anywhereinmaterials which meet the require- aircommerce,exceptaircraftofments of ;173.391(a), (b), or (c) of this United States registry under leasetosubchapter in effect on May 3. 1979. and operated solely by foreign nation- (7) Oxygen, or any hazardous mate- als outside the United States. rial used for the generation of oxygen, carried for medical use by a passenger ; 175.10Exceptions. in accordance with 14 CFR 121.574or 135.114. (a) This subchapter does not apply (8) Human beings and animals with to an implanted medical device, such as a (1) Aviation fuel and oil in tanksheart pacemaker, that contains radio- that are in compliance with the instal-active material or with radio-pharma- lation provisions of 14 CFR. Chapterceuticals that have been injectedor in- 1. gested.

LEGEND 28.Excerpt from CFR 49 Part 175.

158 28 Appendix 2

EXCERPT FROM CFR 49 PART 175 Chapter 1Research and Special Praire nts Administration § 175.30 (9) Smoke grenades, flares, or simi-diet and, at all times be, under the lar devices carried only for use duringcontrol of a blaster who is licensed a sport parachute jumping activity. under a state or local authority identi- (10) Personal smoking materials in-fied in writing to the FAA district tended for use by any individual whenoffice having jurisdiction over the op- carried on his person except lighterserator's certificate, if any, or the FAA with flammable liquid reservoirs andregional office in the region where the containers containing lighter fluid foroperator is located. use in refilling lighters. (49 U.S.C. 1803. 1804. 1806. 1808; 49 CFR (11) Smoke grenades, flares, and py- 1.53 and App. A to Part 1) rotechnic devices affixed to aircraft (Arndt. 175-1. 41 FR 16106. Apr. 15. 1976. as carrying no person other than a re-amended by Arndt. 175-1A. 41 PR 40686. quired flight crewmember during any Sept. so. 10703 flight conducted at and as a part of a Nary For amendments to i 175.10 see the scheduled air show or exhibition ofList of CFR Sections Affected appearing in aeronautical skill. The affixed installa- the Finding Aids section of this volume. tion accommodating the smoke grenades, flares, or pyrotechnic devicesf 175.20C,ompliaart. on the aircraft must be approved by Unless the regulations in this sub- the FAA for its intended use. chapter specifically provide that an- (12) Hazardous materials which areother person must perform a duty. loaded and carried on or in cargo-onlyeach operator shall comply with all aircraft and which are to be dispensedthe regulations in Parts 102, 171, 172, or expended during flight for weatherand 175 of this subchapter and shall control, forest preservation and pro-thoroughly instruct his employees in tection, or avalanche control purposesrelation thereto. (See 14 CFR 12!.135, when the following requirements are121.401, 121.433a, 135.27 and 135.140.) met: (i) Operations may not be conducted I 175.30Accepting shipments. over densely populated areas, in a con- (a) No person may accept a hazard- gested airway, or near any airportous material for transportation aboard where air carrier passenger operationsan aircraft unless the hazardous mate- are conducted. rial is (ii) Each operator shall prepare and (1) Authorized, and is within the keep current a manual containingquantity limitations specified for car- operational guidelines and handlingriage aboard aircraftaccording to prccedures, for the use and guidance; 172.101 of this subchapter of flight, maintenance, and ground (2) Described and certified on a ship- Personnel concerned in the dispensingping paper prepared in duplicate in ac- or expending of hazardous materials.cordance with Subpart C of Part 172 The manual must be approved by theof this subchapter. The originating FAA District Office having jurisdic-aircraft operator must retain one copy tion over the operator's certificate, ifof each shipping paper for 90 days; any, or the FAA Regional Office in (3) Labeled and marked, or placard- the region where the operator is locat-ed (when required), in accordance with ed. Each operation must be conductedSubparts D. E and F of Part 172 of in accordance with the manual. this subchapter and (iii) No person other than a required (4) Labeled with a "CARGO AIR- flight crewmember. FAA inspector, orCRAFT ONLY" label (see ;172.448 of person necessary for handling or dis-this subchapter) if the material as pre- pensing the hazardous material maysented is not permitted aboard passen- be carried on the aircraft. ger-carrying aircraft. (iv) The operator of the aircraft (b) Except as provided in paragraph must have advance permission from(c) of this section, no person may the owner of any airport to be used forcarry any hazardous material aboard the dispensing or expending operation.an aircraft unless, prior to placing the (v) When dynamite and blastingmaterial aboard the aircraft, the oper- caps are carried for avalanche controlator of the aircraft has inspected the flights, the explosives must be han-package, or the outside container pre-

LEGEND 29.Excerpt from CFR 49Part 175.

29 159 EXCERPT FROM CFR 49 PART 175

1175.33 Mk 49Transportation pared in accordance with 1173.25 ofnationprovided ontheshipping this subchapter which contains thePapers. material, and has determined thatit has no holes, leakage, or other indica- 1175.45Reporting hazardousmaterials tion that its integrity has beencom incidents. promised, and for radioactive materi- (a) Each operator that transports als that the package seal has not beenhazardous materials shall report to broken. the nearest Air Carrier District Office (c) The requirements of paragraph(ACDO), Flight Standards District (b) of this section do not apply toOffice (PSDO), General Aviation Dis- ORM-D materials packed in a freighttrict Office (GADO) or other FAA fa- container and offered for transporta-cility. except that in place of reporting tion by one consignor. to the nearest of those facilities a cer- tAmdt.175-1, 41 FR 16106. Apr. 15, 1976, u tificate holder under 14 CFR Part 121, amended by Amdt. 175-1A, 41 FR 40656,127, or 135 may report to the FAA Dis- Sept. 20. 1976; Amdt. 175-1B. 41 FR 57072.trict Office holding the carrier'soper- Dec. 30. 19761 ating certificate and charged with overall inspection of its operations, by 1175.33Notification of pilot-in-command. telephone at the earliest practicable When materials subject to the provi-moment after each incidentthat sions of this subchapter are carried inoccurs during the course of transpor- an aircraft, the operator of the air-tation (including loading, unloadingor craft shall give the pilot-in-commandtemporary storage) in which asa the following information in writingdirect result of any hazardous materi- before takeoff: al (a) The information required by (1) A person is killed: 11172 -202 and 172.203 of this sub- (2) A person receives injuries requir- chapter; ing his or her hospitalization; (b) The location of the hazardous (3) Estimated cal..c., or other prop- material in the aircraft; and erty damage, or both, exceeds $50,000; (c) The results of the inspectionre- (4) Fire, breakage, or spillage orsus- quired by 1175.30(b). pected radioactive contamination occurs involving shipment of radioac- (Arndt. 175-1A. 41 FR 40656.Sept.20. 1576) tive materials (see1115.700(b)): (5) Fire,breakage, spillage, or sus- *17525 Shipping papers aboard aircraft. pected contamination occurs involving (a) A copy of the shipping papersre-shipment of etiologic agents. In addi- quired by 3 175.30(aX2) mustaccompa-tion to the report required bypara- ny the shipmentitcovers duringgraph (a) of this section, a reporton transportation aboard an aircraft. an incident involving etiologic agents (b) The documentsrequiredby para-should be telephoned directly to the graph (a) of this section and 3 175.33Director. Center for Disease Control, may be combined into oae document ifU.S. Public Health, Atlanta, Georgia, itis given to the pilot-in-commandarea code 404-633-5313; or before departure of the aircraft. (6) A situation exists of sucha nature that, in the judgment of the 1175.40 Keepingand replacement ofcarrier, it should be reported to the labels. Department even though it does not meet the criteria of paragraph (b)(1), (a) Aircraft operators who engage in(2), or (3) of this section,e.g., a con- the transportation of hazardousmate-tinuing danger to life exists at the rials must keep an adequate supplyofscene of the incident. the labels specified in Subpart Eof (7) If the operator conforms Part 172 of this subchapter,on hand to the at each location where shipments provisions of this section, the carrier arerequirementsof 1171.15 except loaded aboard aircraft. 1171.15(c) of this subchapter shall be (b) Lost or detached labels forpack-deemed to have been satisfied. ages of hazardous materials must be (b) The following information shall replaced in accordance with theinfor-be furnished in each report:

-4.

LEGEND 30.Excerpt from CFR 49 Part 175. 160" Appendix 2

EXCERPT FROM CFR 49 PART 175

Chapter lRosoarch and Spockd Programs Administration § 175.85 (1) Name of reporting person; (ii) In any freight container within (2) Name and address of carrier rep-an accessible cargo compartment, or resented by reporter. (iii) In any accessible cargo compart- (3) Phone number where reporterment in a cargo-only aircraft in a can be contacted; manner that makes itinaccessible (4) Date, time, and location of inci-unless in a freight container; dent; (3) Packages containing radioactive (5) The extent of the injuries, if any;materials when their combined trans- and port indices exceed 50. (6) Classification, name and quantity (b) No limitation applies to the of hazardous material involvementnumber of packages of ORM material and whether a continuing danger toaboard an aircraft. life exists at the scene. (Arndt. 175-1A. 41 FR 40686, Sept. 20. 1976) (c) Each operator who transports hazardous materhis shall report in1 175.78 Stowage compatibility of cargo. writing, in duplicate, on DOT Form F (a) No person may stow a package of 5800.1 within 15 days of the date ofa corrosive material on an aircraft discovery, each incident that occursnext to or in a position that will allow during the course of transportationcontact with a package of flammable (including loading. unloading, or tem-solids, oxidizing materials, or organic porary storage) in which. as a directperoxides. result to hazardous materials, any of (b) No person may stow a package the ercumstances set forth in para-labeled BLASTING AGENT on an air- graph (a) of this section occurs orcraft next to, or in a position that will there has been an unintentional re-allow contact with a package of special lease of hazardous materials fromafireworks or railway torpedoes. package. Each ''operator making a report under this section shall send (Arndt. 176-1, 41 PR 16106. Apr. 15, 1976, as that report to the Materials Transpor- amended by Amdt. 175-6, 44 FR 31134. May tation Bureau, Office of Hazardous 31. 1979) Materials Regulation, Department of1 175.79 Orientation of cargo. Transportation, Washington, D.C. (a) A package containing hazardous 20590. with a separate copy to thematerials marked "THIS SIDE UP ", FAA facility indicated in paragraph"THIS END Up-, or with arrows to in- (a) of this section. dicate the proper orientation of the (Arndt. 175-1. 41 FR 16106. Apr. 16, 1976. as package,mustbestored,loaded amended by Amdt. 175-1A. 41 FR 40636.abroad an aircraft in accordance with Sept. 20, 1976) such markings, and secured in a manner that will prevent any move- Subpart IILoading, Unloading and ment which would change the orienta- Handling tion of the package. (b) A package containing liquid haz- 4175.75 Quantity limitations aboard air-ardous materials not marked as indi- craft. cated in paragraph (a) of this section must be stored and loaded with clo- (a) Except as provided in I 175.85( b).sures up. no person may carry on an aircraft (1) A hazardous material exceptas 4 175.85 Cargo location. Permitted in Part 172 of this sub- (a) No person may carry a hazardous chapter; material subject to the requirements (2) More than 50 pounds net weightof this subchapter in the cabin ofa of hazardous material (and in additionpassenger-carrying aircraft. thereto. 150 pounds net weight of non- (b) Each person carrying materials flammable compressed gas) permittedacceptable only for cargo-only aircraft to be carried aboard passenger-carry-shall carry those materials in a loca- ing aircraft tionaccessibletoa crewmember (I) In an inaccessible cargo compart-during flight. However, when materi- ment. als acceptable for cargo-only orpas- 1

LEGEND 31. Excerpt from CFR 49 Part 175.

31 i 161

IMNIMI1.1.6.111... AppondIX 2

I EXCERPT FROM CFR 49 PART 175

1 17540 Title O.Transportation

senger carrying aircraft are carriedon (Amdt. 175 -1, 41 FR 16106, Apr. 15, 1976,as a small, single pilot, cargo-only air-amended by Amdt. 175-1A. 41 FR 40606. craft being used where othermeans of Sept. 20, 19761 transportation are impracticableor not available, they may becarried 11175.90 Damaged shipments. without quantity limitationas speci- Except as provided for in f 175.700, fied in f 175.75 in a location thatIs notthe operator of an aircraftshall accessible to the pilot subject totheremove from the aircraft any package following conditions. subject to this subchapterthat an- (1) No person other than thepilot,pears to be damaged or leaking. No an FAA inspector, the shipperor con-person shall place or transport a pack- signee of the material or a representa-age that is damaged or appears to be tive of the shipper or consigneeso des-damaged or leaking aboardan aircraft ignated in writing, or aperson neces-subject to this Part. sary for handling the material may be (Arndt. 175-1, 41 PR 16106, Apr. 15, 1976,as carried on the aircraft. amended by Arndt. 175-1A, 41 PR40666. (2) The pilot must be providedwith Sept. 20, 19761 written instructions on characteristics and proper handling of the material. Subpart CSpocific R. bons Ap- (3) Whenever a change ofpilots plicable Aswan to Classiffeation occurs while the material is on board, of Material the new pilot must be briefedunder a hand-to-hand signature servicepro-I175.305Self-propelled vehicles. vided by the operator of theaircraft. (a)Self-propelledvehiclesare (c) No person may load magnetizedexempt from the drainage require- material (which might causean erro-ments of 1173.120 of this subchapter neous magnetic' compass reading)onwhen carried in aircraft designedor an aircraft, in the vicinity ofa mag-modified for vehicle ferry operations netic compass, orcompass master unit,and when all of the following condi- that is a part of the instrumentequip-tions are met: ment of the aircraft, ina manner that (1) Authorization for this typeoper- affects its operation. If thisrequire-ation has been given bythe appropri- ment cannot be met, a specialaircraftate authority in the governmentof swing and compass calibrationmay bethe country in which the aircraftIs made. No person loadingmagnetizedregistered; materials may obscure thewarning (2) Each vehicle is secured inan up- labels. right position; (d) No person maycarry materials (3) Each fuel tank is filled ina subject to the requirementsof thismanner and only to a degree that will subchapter in an aircraft preclude spillage of fuel duringload- unless theying,unloading, and transportation; are suitably safeguarded topreventand their becoming a hazardby shifting. For packages bearing "RADIOAC- (4) Ventilation rates to bemain- TIVE YELLOW-II"or "RADIOAC-tained in the vehicle storagecompart- TIVE YELLOW-III" labels,such safe-ment have been approved by theap- guarding must prevent movement propriate authority in thegovernment thatof the country in which theaircraft is would permit the packageto be closerregistered. to a space that is occu piedby a person or an animal than is permittedby'175.310 Transportationofflammable I 175.700. liquid fuel in small, passenger-carrying (e) No person may carrya material aircraft. subject to the requirementsof this A small aircraft or helicopter subchapter that is acceptablefor car- operat- riage in a passenger-carrying ed entirely within the Stateof Alaska aircraftor into a remote area elsewherein the (other than magnetizedmaterials)United States maycarry, in other unless it is located in the aircraftin athan scheduled passenger place that is inaccessibleto persons operations, other than crew-members. not more than 20 gallons offlammable / liquid fuel, if

LEGEND 32.Excerpt from CFR 49 Part 175.

A 62 32 Appendix 2

EXCERPT FROM CFR 49 PART 175

Chapter 1Rosoards and Spode, Programs Administration 1 175.320 (a) Transportation by air is the onlybeen approved by the FAA district practical means of providing suitableoffice responsible for inspection and fuel; surveillance of the aircraft on which (b) The flight is necestAry to meetthe equipment is carried. the needs of a pummel; (d) In the case of a helicopter, the (c) The fuel Is carried in metal containers that ue either fuel is carried on external cargo racks; (1) DOT Specification 2A containers (e) The area or compartment in of not more than 3 gallons capacity,which the fuel is loaded is ventilated each packed inside a DOT Specifica-so as to prevent the accumulation of tion 12B fibuboard box or each fumes; packed inside a DOT Specification (f) Before each flight, the pilot-in- 15A, 15B, 15C. IMAM or 193 woodencommand box, or in the case of a small aircraft (1) Informs each passenger of the lo- inAbel's, each packed Inside acation of the fuel and the hazards in- wooden box of at least one-half inchvolved; and thickness: (2)Prohibitssmoking,lighting (2) Airtight, leakproof, inside con-matches, the carrying of any lighted tainers of not more than 10 gallons ca-cigar. Pipe. cigarette or flame. and the pacity and of at least 28-gauge metal, use of anything that might cause an each packed inside a DOT Specifica-open flame or spark, while loading or tion 15A, 1513. 15C. 16A, 19A, or 193unloading or in flight; and wooden box or. in the case of a small (g) Fuel is transferred to the fuel aircraft in Alaska, each packed insidetanks only while the aircraft is on the a wooden box of at least one-half inch surface. thidmerg (Arndt 175-1. 41 FR 10106, Apr. 15, 1970, as (3) DOT Specification 178 contain- amended by Arndt. 175-1A. 41 PR 406116, ers of not more than 5 gallons capac- Sept. 20. 1970) ity: or (4) Fuel tanks attached to flamma- ;175.335 Cargo-oaly aircraft; only mesas ble liquid fuel powered equipment of transportatiom under the following conditions: (a) Notwithstanding 1 172.101. when (i) Bach piece of 'equipment is se-means of transportation other than cured in an upright position; air are impracticable or not available. (ii) tech fuel tank is filled inahazardous materials listed in the fol- manner that will preclude spillage oflowing table may be carried ona fuel during loading, unloading, andcargo-only aircraft subject to the con- transportation; and ditions stated in the table and in para- (111)Ventilationrates which aregraph (b) of this section and whenap- maintained in the compartment inpropriate, paragraph (c) of thissec- which the equipment is carried havetion:

PAsos1elssorlplon Cams Catalans

Mine Rasing cogn Om, Pus A nsploskss Pena*, any when no (NW situ is Ow; Me *Irma How- awl 1.000). sm. Ito Oscine 00111,0 asps are oohed in en IME 02 eon. War Res de CFR 171.7(0(0), ass mos as ansponsel In the sow skss11 sillh melmIsh OW are nol dossed in howdous nonsolis. Swift Moire sops Clore C ssoloshis Pamilsd only *ten no crier woo Is shard Me Won% How (1.000 of less) awn, 11 11. OMR IWO. ape so maul Ina LtOT MC 001 owl** 141 CPS 1753110 or an Re U online, pm RI CFR 171.760011 mss rap as 1nsepoRsi In its Isms slash WM oslelsIs oast Om dus A or cams 11 ospkokes. PsrollIsd in NAN aims horns Ws/ olpacass al SG el of Ws. liss est W 1ranumns0 In as we It- crs0slit wanes ROSIN so dm A, II. of C sn- olodsss. Waal spnlo. woke MOW Of0* 111111 nhaSsIsOL Psmelsel In MOM Isrdis ma hsvins a oes011y al moto 0110 110 .1 NOW lo Me osedlOws spsolOs0 in vets. (a) of Inis melon.

LEGF.IC 33.Excerpt from CFR 49 Part 175.

33 . 1 6 3 EXCERPT FROM CFR 49 PART175 II171.320 NI* 4,--Transportation

MOWN tlewseshn Oen Conditions Kph .cobras Ors A apemen WOWS to ego** to be wad tor blue* Peewit- led only when no Mee cep is aboard Meaimatt or seen being transeeted in Mw woe sinwatt willt en mew** Wpm* el aye 1 or more el SSW N. Wane me lsese by be used* Welty Mnroorean neele-eal el Nam Illsolne sew* n.o.s. Conine *Nowt kW Propolent ..cobra footle Mrs (re* sots one). loweelent meioses weld) doss II helmpee mei). 011 n.o.s.: patrolmen ce or Flonenoble bosid. peedeent at n.o.s. estmlese in mate Owns hoeing mud copse*. of SS tost or loss. Mss not be trepotled in Is mme ele met with msbetis dewed as elms A. ILOf C Oh 111016,10, blasting seetes, cameo malsoels.or owl dIstne tnoWials. Peoneled in MOW Wee *eh Movie e a sopeolty of more tan 110 piOubild to Ma sondem ape celed in tem Kt) al the ma= Combs Ibis lipid. n.os Contuse* herd ...... Nee** in instead us each havinga ospsoNy GO more San 110 991 *bled to the conditions opecible NOM in par. (c) el Ilds (b) The following conditions applycraft and its operation in takeoff.en to the carriage of hazardous materialsroute, and in landing must be performed under the authority of conduct- thised at a safe distance from heavilypop- section: ulated areas and fromany place of (1) No person other thana requiredhuman abode or assembly. flight crewmember, an FAA inspector, (5) If the aircraft is being the shipper or consignee of themateri-by a holder of a certificateoperated al or s reprezentative of the shipperor issued consignee so designated in writing, under 14 CFR Part 121, Part127. or or Part 135, operations must beconduct- a person necessary for handling theed in accordance with material may be carried on theair- conditions and craft. limitations specified in thecertificate holder's operations specifications (22 The operator of the aircraftmust or have advance permission from theoperations manual accepted bythe owner or operator of each manned air-FAA. If the aircraft is beingoperated port where the material is to be loadedunder 14 CFR Part 91.operations or unloaded or where the aircraft is tomust be conducted in accordancewith land while the material is an operations plan accepted andac- on board.knowledged in writing by theopera- When the destination is changed aftertor's FAA District Office. departure because of weather or other (6) Each pilot of the aircraftmust be unforeseen circumstances, permissionprovided written instructions from the owner or operator of theal- stating ternate airport should be obtained the conditions and limitationsof the asoperation being conducted andthe soon as practicable before landing. name of the airport officials] grant- (3) At any airport where theairport owner or operator or authorised lag the advance permissionrequired repre-by the first sentence ofparagraph sentative thereof has designateda lo-(bX2) of ;his section. cation for loading or unloadingthe (7) The aircraft and the material concerned, the materialmay loading ar- not be loaded or unloaded atany otherrangement to be used must beap- location. proved for safe carriage of theparticular materials concerned bythe FAA (4) If the material concernedcanDistrict Office holding the create destructive forcesor have lethal operator's certificate and charged withoverall in- or injurious effects overan apprecia-spection of its operations, ble area as a result ofan accident in- or the ap- volving the aircraft propriate FAA District Officeserving or the material,the place where the materialis to be the loading and unloading ofthe air-loaded.

LEGEND34.Excerpt from CFR 49 Part 175.

16434 Appendix 2

EXCERPT FROM CFR 49 PART 175

Chapter ISseareh and Special Programs Administration § 175.700 (8) When Class A explosives are car-combustible liquid from a container, ried under the authority of this sec-other than an approved bulk tank, tion. the operator of the aircraft shallwhile that container is insideor within obtain route approval from the FAA50 feet of the aircraft. inspector in the operator's FAA Dis- (iv) When filling an approved bulk trict Office. tank by hose from inside the aircraft, (9) During loading and unloading, nothe doors and hatches must be fully person may smoke, carry a lightedopen to insure proper ventilation. cigarette, cigar, or pipe, or operate any (v) Static ground wires must be (....1- device capable of causing an opennected between the storage tank c r flame or spark within 50 feet of thefueler and the aircraft, and betweel aircraft. the aircraft and a positive ground (c) The following additional condi- device. tions apply to the carriage of flamma- (Arndt 175-1, 41 FR 16106. Apr. 15, 1976, as ble liquids and combustible liquids inamended by Arndt. 175-1A. 41 FR 40686. tanks each having a capacity of more Sept. 20, 1976] than 110 gallons under the authority Non: For amendments to I 175.320 see of this section: the List of CPR Sections Affected appearing (1) The tanks and their associated in the Finding Aids section of this volume. Piping and equipment and the installa- I 175.430 tion thereof must have been approved Special requirements forpoi- for the material to be transported by 1101116 the appropriate FAA Regional Office. (a) No person may transport a pack- (2) In the case of an aircraft beingage bearing a POISON label aboard an operated by a certificate holder, theaircraft in the same cargo compart- operator shall list the aircraft and thement with material which is marked approval information in its operatingas or known to be food stuff, feed, or specifications. If the aircraft is beingany other edible in labia intended for operated by ether than a certificateconsumption by husuans or animals. holder, a copy of the FAA Regional (b) No person may operate an al. Office approval required by this sec-craft that has been used to transport tion must be carried on the aircraft. any package bearing a POISON label (3) The crew of the aircraft must beunless, upon removal of such package, thoroughly briefed on the operation ofthe area in the aircraft in which itwas the particular bulk tank system beingcarried Is visually inspected for evi- used. dence of leakage, spillage, or other (4) During loading and unloadingcontamination. All contamination dis- and thereafter until any remainingcovered must be either isolated or re- fumes within the aircraft are dissipat-moved from the aircraft. The oper- ed: ation of an aircraft contaminated with (i) Only those electrically operatedSUM poisons is considered to be the bulk tank shutoff valves that havecarriage of poisonous materials under been approved under a supplementalparagraph (a) of this section. type certificate may be electricallyop-I175.440 Special requirements for other erated. regulated materials. (ii) No engine or electrical equip- Asbestos mutt be loaded, handled, ment, avionic equipment, or auxiliaryand unloaded, and any asbestos con- power units may be operated, excepttamination of aircraft removed, in a position lights in the steady positionmanner that will minimise occupation- and equipment required by approvedal exposure to airborne asbestos parti- loading or unloading procedures,as setcles relersed incident to transporta- forth in the operator's operationstion.(Seet .73.1090ofthissub- manual, or for operators thatare notchapter.) certificate holders, as set forth ina written statement. (Arndt. 175-7. 43 FR 56668, Dec. 4. 1978] (iii) No person may fill a container, 1175.790 Special requirements for radio- other than an approved bulk tank, active materials. with a flammable orcombustible (a) No person may place any pack- liquid or discharge a flammableorage of radioactive materials bearing

LEGEND 35.Excerpt from CFR 49 Part 175.

tn 35 165 lkrijigr,r.ji...... y...,...... _._..-,-,..- EXCERPT FROM CFR 49 PART 175 175.700 Title 49Transportation "RADIOACTIVE YELLOW-LI" orfollowing table to any packagecon- "RADIOACTIVE YELLOW-III" labelstainingundevelopedfilm(ifso in an aircraft closer than the distancesmarked). If more thanone of these shown in the following table toa apacepackages is present, the distance shall (or dividing partition between spaces)be computed from the following table which may be continuously occupiedon the basis of the total transport by people, or shipments of animals,orindex numbers shown on labels ofthe closer than the distances shown intheindividual packages in the aircraft:

Minimum Mournum eeperelion defences m feet dielarme m Nat 10 Is merest undeveloped fern for venom 10 Mee of emu of ranee Total Ireneporl Mee moon& or minimum disarms m lilt lo 2 Iv2-4 hr 4-6 tir -121r Over from &Min 1217 perINce of cow tempar1ment None 0 0 0.1 lo 1.0 .. 0 0 0 0 1 2 3 1.1 10 5.0 4 5 1 3 4 6 11 4 6 9 10.1 lo 20.0 11 15 3 5 6 20.1 lo 30.0 12 16 22 4 7 10 30.1 lo 40.0 15 20 29 5 11 40.1 lo 50.0 17 22 33 9 12 19 24 39 7 (b) In addition to the reportmk,re- (c) No person maycarry aboard a quirements of I 175.45, thecarrier must also notify the shipperat thepassenger-carrying aircraft any pack- earliest practicable moment followingage of radioactive material whichcon- any incident in which there has beentains a large quantity (largeradioac- tive source) of radioactivity(as de- breakage. spillage, or suspectedradio-fined active contamination involving radio- in 173.389(b)ofthis sub- active materials shipments. Aircraftinchapter), except as specificallyap- proved by the Director, Officeof Has- which radioactive materials havebeenardous Materials Regulation, spilled may not be again placedin Materi- service or routinely occupied untiltheals Transportation Bureau.Depart- radiation does rate at any accessiblement of Transportation. surface is less than 0.5 milliremper (d) Except as provided inthis para- hour and there is no significantre-graph, no person maycarry aboard a movable radioactive surface contami-passenger-carrying aircraft any radio- nation (see$ 173.397 of thissub-'active material other thana radioac- chapter). In these instances, thepack-tive material intended foruse in, or in- age or materials should be segregatedcident to, research or medicaldiagno- as far as practicable from personnelsis or treatment. Prior to May3, 1981, contact. If radiological adviceor assist-this prohibition does not applyto ma- ance is needed, the U.S. Energy Re-terials which meet therequirement. search and Development Administra-of I 173.391(a), (b),or (c) of this sub- tion should also be notified. Incase ofchapter in effect on May 3, 1979. obvious leakage, or if itappears likely that the inside containermay have(49 U.S.C. 1803, 1804, 1808. 1808; 49CPR been damaged, care should betaken to 1.53 and App. A to Part 1) avoid inhalation, ingestion, or contact lAindt. 175-1. 41 FR 18108. Apr. 15, 1978.as with the radioactive materials.Any amended by Amdt. 175-4, 42 FR 22387.May loose radioactive materirls shouldbe 3, 19771 Oil in a segregated area pending dis- posal instructions from qualifiedper- Non: For amendments to 1175.700see sons. the List of CPR Sections Affectedappearing in the Finding Aids section of thisvolume.

LEGEND 36.Excerpt from CFR 49 Part 175.

166 36 Appendix 2

EXCERPT FROM CFR 49 PART 175

Chapter 1Rosaarch and Spacial Programs Administration § 175.710 i 175.710Special requirements for fissile (2) On any aircraft on which there is Class III radioactive materials. no other package of radioactive mate- (a) No person may carry aboard anyrials required to bear one of the itA- aircraft any package of fissile Class III DIOACTIVElabels describedin radioactive material (as defined in II 172.436, 172.438, and 172.440 of this I 173.389(aX3)ofthissubchapter),subchapter.Specificarrangements except as follows: must be effected between the shipper (1) On a cargo-only aircraft whichand carriers, with instructions to that has been assigned for the sole use ofeffect issued with the shipping papers; the consignor for the specific ship-or ment of fissile radioactive material. (3) In accordance with any other Instructions for such sole use must beprocedure specifically approved by the provided for in special arrangementsDirector, Office of Hazardous Materi- between the consignor and carrier,als Regulation, Materials Transporta- with instructions to that effect issuedtion Bureau. with shipping papers: cr. (Arndt. 175-1. 41 FR 16106. Apr. 15. 1976. as amended by Amdt. 175-6. 43 FR 48645. Oct. 19. 19781

LEGEND 37.Excerpt from CFR 49 Part 175.

167 37 : -A Appendix 2 PIREP

914! IOCIVitHENOMENA 3=LTRIDENT FL /SK RADIAL DISTANCE TIME (Z) FLT LVL SKY OVER BASEAMOUNT TOP AMIP- ...CELSIUS ii I ND., DIRECTION SPEED /TB"- l'URBULENCEINTINSITY TYPE* ALTITIDE** TYPEALT.ITUTIF**

k3S MOST HAZARDOUSiLEME it

LEGEND: .110... SPACE SYMBOL MIIIM *ONLY FOR CAT ***ONLY IF DIFFERENT FROM FL ares di,. se s INTINSIIT ar.ICI ACCUMULATION I TURBULENCE REPORTING CRITERIA TABLE beer Ice becomes perceptible. Rate of accumulation slightly greater than rate of sublimation. Intensity Aircraft Reaction It Is not hasardous even though deicing/ Reaction Inside Aircraft nntl-icing equipment is not utilised, unless Turbulence that momentarily causesOccupants may feel a slight encountered for an extended period of time slight,erratic changes in altitude (over 1 hour). and/or attitude (pitch, roll, yaw).strain against seat belts or Report asLight Turbulence: shoulder straps. Unsecured light The rate of accumulation may create a problem Ifflightis prolonged in this or LIGHT or objects may be displaced vironment (over 1 hour).Occasional use of slightly.Food service may deicing/anti-Icingequipment removes/ Turbulence that causes slight, rapid preventsaccumulation.It does not present and somewhat rhythmic bumpinessbe conducted and little or problem it the deicing/anti -icing equipment ,ikout appreciable changes In sill- Is used. no diMculty is encountered de or attitude.Report asLight hop. In walking. Merrier. The rate of accumulation is such that even short encounters become potentiallyhaz- ardous and use of deicing/anti-icing equip- Turbulence that Is similar to LightOccupants feeldefinite Turbulence but of greater intensity.strains against seat belts or ment or diversion Is necessary. Changes In altitude and/or attitudeshoulder straps. Unsecured occur but the aircraft remains In objects are dislodged. Food Severe The rate of accumulation Is such that positive control atalltimes. Itservice and walking are dif- Icing /anti -icing equipment fails to reduce o usually causes variations Inbull- (knit. control the hazard.Immediate divenlon rated airspeed. Report asModerate Turbulence:I necessary.

MODERATE or Pilot Report: Aircraft Identification, Location,Time (GMT), Intensity of Tyne, Altitude/FL, Aircraft Type Turbulence that Is similar to Light IAA and OAT

Chop but of greater intensity.It 40,11, causes rapid bumps b.- jolts with- AI out appreciable changes in aircraft FORECAST WINDS AND TEMPERATURES ALOFT altitudeorattitude. Reportas Moderate Chop. (FD) Interpretation 12° C,wind060°at5 knob Turbulence that caurlarge,air- Occupants are forced vio- rupt changesInriseviletand/orlently against seat belts or attitude. It wanly causeslarge shouider straps. Unsecured 3° C,wind160°at25knots SEVERE variations in Indicatedairspeed. objects aretossedabout. Aircraft may be momentarily outFood service and walking of control.Report as Revere TIlr, are impossible. brience. \. -09 Turbulent* la which the aircraft Is 9° C.wind260°atSOknots violently tossed about and isPrim- EXTREME Orally impossibletocontrol. It may cause structural damage.Re- port asRetreatsTurealeisoe. 47° C,wind360° at 115 knots Elsa heel turbulence Normally abwre.15,000 feet -4T Leeriness. AIM) not emochited with rumuliform Iaehmthei Mamilenteeme, dwelt, be reported as CAT Weer sir turbulence) preceded ty bie appropriate latenelty, or light or moderato elwp. 11° C, wind elm (light 99 variable)

LEGEND 38.-PIREP.

168 38 WIND ECHO PRECIPITATION POSSIBLE HAIL LIGHTNING LEVELINTENSITY INTENSITY TURBULENCE GUSTS

1 LIGHT LGT/MDT WEAK , 1.....2 MODERATE MODERATE LGT/MDT

3 STRONG HEAVY SEVERE VERY VERY SEVERE POSSIBLE POSSIBLE YEe N4 STRONG HEAVY K--5 I Na iENSE INTENSE SEVERE ORGANIZED LIKELY YES 450 6 EXTREME EXTREME SEVERE EXTENSIVE LARGE YES Highest precipitation tops in1 area in hundreds of feet. * The numbers representing the intensity level do not appear on the chart. Beginning from the first contour line, bordering the area, the intensity levelis 1-2; second contour is 3-4; and third contour is 5-6. SYMBOLS USED ON CHART SYMBOL MEANING SYMBOL MEANING SYMBOL MEANING

R RAIN + ' NTENSITY INCREASING RW RAIN SHOWERS OR NEW ECHO LINE OF ECHOES A HAIL - INTENSITY DECREASING 1 NO OVER 9/10 COVERAGE IN S SNOW NO CHANGE SLD IP ICE PELLETS SYMBOL A LINE SW SNOW SHOWERS W5991 CELL MOVEMENT TO NE THUNDERSTORM WATCH L DRIZZLE 35 T THUNDERSTORM AT 35 KNOTS TORNADO WATCH ZR, ZL FREEZING PRECIPITATION FWT99T NE NO ECHOES OBSERVED 46--0.LINE OR AREA MOVEMENT NA OBSERVATIONS UNAVAILABLE TO EAST AT 20 KNOTS LEWP LINE ECHO WAVE PATTERN OM OUT FOR MAINTENANCE STC STC ON -- all precipitation MA ECHOES MOSTLY ALOFT may not be seen PA ECHOES PARTLY ALOFT

LEGEND 39.Key to Radar Summary Chart. 169 170 APPENDIX 3

171 Appendix 3

Perm Amend OMB No IMO* 1.11011PARTIMINT OF TRANIPONTATION TIMESTARTED MUM maw Mar= AgerismeMON (FAA USE ONLY) 0 PILOT BRIEFING 0 VNR FLIGHT PLAN 0 STOPOVER

1 2 Amour! 2AVICRAPT ME/ TnuE 5 DEPNITuPIE POINT 6 Otesterurs tea IDINTOCATION SPICY. SOUITIMPIT AIRSPEED 7 ALTITUDE PTIOpOSED (Z) ACTUAL It) )( W/13 LAX FL .27 0 DWI 3erifit MI $ROUTE Os Kett LAX FLIPR2,TRM316q sALAM oirsALori.ARLiss 5swelanerepdgivi. 1. err rest Omura 11 nitMllite Nom aaNl,rEa Patmix I P IL OltSONO 13ALTESNATE AITIPOST(S) 64PILOTS NAME AOCNESS TELEPHONE WPM I orICRAFT HOME SAIL is Nome NOUNS MINIM AWARD

WA"DESTINATIONCONTACMILEPHONE (OPTIONAL) Pc

pCOLON OP AinCsien CIVIL /MCNAIR PILOTS. FAA Pen lk nowirow Pen Ms EnIFR SISTOOenID 0511*under instrument Mete ruins in cool Girspeos Plana Ns =id mull in eate MAW/nal10weedPADTerWSTIESESon (SedIsnKa of We PedErslAviebenMOP 1115S.as amended)Film. GI a VOA INghlplanIsleccernended esa gOod oporawrypreebes&soft Pan IS kw wwwWwwasksmown",OVFN SOW pans FM Form 7233.1te4e) CLOSE VFR FLIGHT PLANWITH FSS ON ARRIVAL FLIGHT LOG

CHECK POINTS ROUTE MACH WIND SPEED-KTS DIST TIME FUEL

FROM TO ALTITUDE NO TEMP TAS GS NM LEG TOT LEG TOT

LEVEL FLIPR * LAX OFF CLIMB :19 4400

LEVEL J169 330/45 TRM OFF FL 270 ISA -2 21

11 J169 TRM BLH 330/4.: FL270 ISA -2 . SALOM J169 340/42 BLH INT FL270 ISA -2 SALOM PHX 1NT DESCENTAND A7PROACH :10 1250

OTHER DATA:* Includes 1,000 lbs fuel for taxi. FLIGHT SUMMARY NOTE: Use 10,500 PPP fuel from level off to I. TIME FUEL SALOM INT. EN ROUTE RESERVE Use 9,400 PPH fuel flow for reserve -- 1200MISSED APPR. requirements. TOTAL

FIGURE1. FlightPlan/Flight Log.

1 172 L ANOOSLES INTL UPR TWO DEPARTURE (PILOT NAV) LOS ANOEUrS, CAUFOINIA CALIFORNIA 42 MS fit 1112 DADAGOTW. 136.63 LOS ANGELES Chen AP ..r,:s...r.'01 00.11%r 014C Olt Lamas INTL 6A10 95W UTC-9(-707) 33'56'33'N 118'24'26"W 121A 327.0 1434.ST.7S'-41166S4 64 l 126 11 54 OWL 100, JET A OK 4 1.44, NI N34.28.44/ OND CON LRA CfR Indst E 121.15 (N) 121.71 (5) 327.0 W11728.11' ~URA LOS MOMS TOWER IIIRWL21 N12131E150 (CONC411110) 6175. 11-225, 01400. 001-900 1551. CL 108.2 WU 'IL,'" S 120.55 5711.1 WNW WM. VAS(141.)-(1A 2.5'TOI 59'. WWI% Rot tic. Own N 131.11 235,) Mat MAUR. Taid dopka want LOS MOUES DEPOON WORM N110901200 (comoonvo) S-175,11225, DT- 400.001100 MIRL Cl SEM MACH 1M:r 355.4 LOS ANGELES. -- . .- Hs 7 met.. WIWI! WM. VA8041)-GA 3.3To4 56.34'. to IM 113.6 LAX Urn Oren 104 111,1211z min TOS Rallreat Chen W 77-..MAT:ilLiaKii WIT WWI: 11102855150 (AWN-COW-GRUM S-110. 0-200. 01-325. 001-750 HURL lia2TTHrvAlmi WNW MAUR. VOW(MO-Uppr GA 3.25'TOI . Lower GA 3.0104 60' Thld &pled 321'. sia. per44.4a Chin 105 01341: WWI. Rot IL. -116--- Wt t735.5, 1111111111.4* N99255150 (001104211166 5-175.0.225. DT-400. 001-900 HIM CL ..r . , . LA 14 WWW: IMLIR. VAII(V61.)-Upow W 3 25'10494'. Low GA 3 0'101 54' .., , WWI* ALSF2. TOL Si Rd W 1.1. (72) ..:1N IN MINOT IMINNik AtImiled catimmudy. Use ahem CAUTION-tubulence nip be deflected upward from to Met ..' \' fence 160' E.1 Ray 25R. CAUTION. Impoirad tang clearance way ad on tramp J behvesn 30K and 1911 When MANX Mane K accupsik 165' osnierNne Is ambalsne Twr PA Writs Nom sent. aryl. On Insbaly tholls no turns FUN `..."4111t (4) 1,12NA?LS NUM before amiss shorties. Ow ':ea apcle utred 0806143021. Roy 245 ALSF2 sprain as MLR DI water N33.3742' i pa blew Mt Ray 251. AU.opersess as MAUI unW weather pas balms VFR Roy 071.255 FAA strut. N114'16.57' Os rani 116 ii4o.wipsw. v ) w 11 r43.41' alf"'OM smiusbox 00.1610 540.000 as, DC-1630 600.000 bs, 1-1011 600.000 61 8747-1W *WOW W. Rwl061-245 FAA gamy avaluNIP 0C-1610 430.000 6s. 0C-1630 510.000 IP, 1-1011 510.000 as. R46076251 FM a 1159all Math melustion DC- 10-10400,000 as. DC-10-30500,000 lbs, 1-1011 600.000IP 11747-SP 710,000135. Roy d 0611241. FM swim meiustion OC-1610 310.000 as, LIC-103040,000 as, L- 1011160,000 at. Da Pest 1%41 /WON 200,000 Bp Wel Warn wheel up to 350.000 as and double dual is den wheel up b 634,000 Ns and 0C10-10 11430.000 as, OCIO-30 t. 576.0001P and 1-1011 to 446.000 mewl A-300 is 314.000 M raga* tarotia, I (42) ail 1725.2ak apt on al nap. A 70015500'slaaway I. Pen ostablIshed at west and of Rwy 241. Numererm bads an and M / ESTI vicinity M sayer( P104 Nelikalion Sento POWS) spiel* SANTACATA(.1144 1. 111.4 sxclig LIT is SI= ily.43 -t .L2...... ," IIG11MLAILL1011010 LLWAS. Chen St Oren 100 CIMMIIIKSIMI*WONNIAL 133.8 WSW 135.65 (213)6462297 KIWI 122 95 N3243.77---0,sa., L.' WW22.50.-1611825 14' Wt14.44' w 1 1 003Ir raw 10101111 PIS (MI6 LC 644-1020. NOTAM FIE IM. L-3.112 w11723.01' VP 121.5 (045'4111r), 124.9(010'424'1 124 5 (225'-044') Tam 133.9(N. pmelmg, 12695 (S. comps°. 119 $120.35 thelicoplms). MON 121.75 (3. onvoing, 121.65 (t4. canna* UMW 121.4 PPEWAL SD Is= 125.2 (249'444') 124.3 (065.440') MISSION SAY 113 gra low =Nape tees VFR Tennis. Area MM. NOTE: Roder required 117.111 WART Chen 106 125 WISAIN10NISISATIO6 NOTAM FILE IM. Th:St WINN 113.1 LAX Chan 83 33'55'53"t4 116'25'52N 132.143' -w 11713.47', fir: r et 61 150/15E N°11:climb 30';erNrAto O. VON uremoble 270480'17-35 NM Wow $000' ";441onin4n;.Own1-3, 11-2- 2110-300'10-20 NM below 5000' INIMINNIMIN 278 OS NOTE Cho,' net se molt 33'57'54"N 118'16'37"W 249'6.2 NM to fld 108.5106S Chen 22 Rey 24R LOW ROMEN NW V Fin, 126 105.3141Q6Chen 22 Roy 241 LOM KONEN NO6 DEPARTURE ROUTE DESCRIPTION ILIMW 109.944( Chen 3611my 251 TAKE-OFF RUNWAYS 24; Climb via heading 250* for vector to WIN 105.9 laN Chen 36 Ray 25R URINE 111.7 SUWU Chen 54 RP/ OK intercept and proceed via VTU R -114 to FUPR INT. Thence.. . . 19/1111 a:1.7 14PE Chan 54 Rwi 065 TAKE-OFF RUNWAYS 23: Climb via runway heading, at LAX 5/1111 III 1 : IAS Chen IS R*7 071 ON 11 IS° 240 VORTAC turn left heading 220' for vector to Interco! and .2', -.....----'""" ' UMW 111.11-511 Chan 411 Rwg 07R proceed via VTU R -114 to FUPR INT. Thence .... f. WIIII011611 (Mt)11 UTC- I( -7DT) 34'15'35"N 115'24'45"W LW MIMS . . via (transition) or (assigned route). Expect further ....4. wows .....!2!n - --- 1004 II 34 MU 10. 1001PA-2004(1000) CCPIIA clearance to filed altitude five minutes after departure. NW 12-3111 14372500 (AWN) n S-15, 0-40 URL LA A DAGGETT TRANSITION (FUP*2.DAG) MI 12 TIP *pad 664' (Unlitted) Nine NWT W Thid dated 490' (Unlighted) Trees Rgt Ik IMPERIAL TRANSITION (FUPIG.IPL) WWII IMMO Wended con/nava* etelacoper op 2500' MSL (1500 AOL) and below C0NIW1CI110N1 CT WII= 122.8 MISSION PAY TRANSITION (FUP112.MIS) 6116110W11111 (14111) LC 842-4817 SANTA CATALINA TRANSITION (FUPR2.SXC) IMO= TO MANX* NOTAM FILE WY 11) TOW/11111 113 1 VW( Chan 78 34'13'24"N 118'29'27"W 046'4 5 NM te IMO 810/15E THEIVAAL TRANSITION (FUP12.TRM) mow 370 PM 34'15'35"N 118'24'45"W st IN (VFR only) NOTAM FILE NW

UPR TWO DEPARTURE (PILOT NAV) LOS ANWILS. LOSANGELECAI 173 PLIPIt2.FLIPR) 174

FIGURE 2.-FLIPR Two Departure (Pilot Nay). PHOENIX UT HARBOR INTL (PHX) ARLIN FIVE ARRIVAL(ARLIN.ARLIN5) PHOENIX, ARIZONA OC BC RWY 26L 4_322 (FAA) MINK ARIZONA PHOENIX APP CON PHOENIX AM CON 121.1 269 6 120.7 393.1 4067 PHOENIX SKY HAWN ATISAIR MIMI TOWER 121.2 120.9 254.3 Flay OM 118.7 3115.4 Ivry Ilt2611 OND CON PHOEM/OUR 121.9 269.2 VALLEY MUNI CINC DEL A22.7 118.1 269 2 9 SCOTTSDALE ADS MR 121.2 W C t 41,0 MUNI DEP 124 3 . 26041 110 6 MIK i Ifr' SALT RIVER n 43 NINTH 115 6 nth.. 1174111.141;7 n I .2704 4111 1 SALON 143.130 vr ICEPRX SKY FALCON LOCAUZER ma ] PHOENDI W113653.29. GOODYEAR HAW* 0411 FIELD 1379 I.PFIX HT," ti. , 3312 ''',,, MUNI V A Chan E. .." 0112 12/1 3000 I:0 4\ e...... 0666* °V° al..64r.5.266 A1511 12/2 25V (6) 1535 A A1471 4100/s_ (Al) ..cy A C..... (4) 0664--8.- STELIAR (221 AMPARK 1565 '1--':== ailiItir ,r1 1369. mom OAF) 0 SEW 1423611 5V WC 2 DME W112641.46' CHANDLER ....4% A Not0I 11 DAVE v. Ievr 13 73 M... MUNI SALT RIVER -.4 115.6 SRP Mi.. REA Chat 103- Chen 1 5 2555 3047 TURBOJET VERTICAL NAVIGATION 11.241 PLANNING INFOR7MM 6000 067011,1 E yetidooranco to cram '... (1 4) By at or Wow 12000'. 10 NM REND MOHAX 1166Ast4Nri 143246 55 Ch an 112 W113651119' BACK COURSE 1.-4,14.2 RADAR REQUIRED .4354

VORTAC sew euv 1111 1-PKR 11 ME ....---7...-' MISSED APPROACH 1.11,14X5 DME Olmb m 3000 then ellnAln. gm NOTE, Chort not to Ka. =,... to 6000 tiredVIP , 15,1°. I MOHAK TRANSITION (MOHAK.ARUN5):From over MOHAK DME FIX via GBN R-247, HADEN I PIG 2 DME BXK R-215 and SRP R-246 to ARLIN INTThence. ... hPHX , ,,4°. 0 5OMR I I SALOM TRANSITION (SALOM.ARLIN5):From over SALOM INT via GBN R-285 and 1151 117.1 1 SRP R-246 to ARUN INT. Thence.... I 112 ....From over ARLIN INTvia SRP R246to SRP VORTAC. Expect radar vectors after as....4 SHIA 1 6 NM 12 11444 To 1121 passing ARLIN INT to finalapproach course. CATEGORY A I C 0 A _ ALL SATELLITE AIRPORTS:Expect radarvectors after crossing ARUN INT. 18042 1800-214 . 11-24, 180e.1 ye 17004) ,g as (7004) 678 (700216) Go WOUND 19041 ess (Tco 1) 1800-2 11110-21/2 256'5.3 NM 118 (7002) 746 (6311216) from VORTAC HADEN ME MINIMUMS r...5 01. i 5404 410 00041 1544114 410 (300116) 1001. Iwy 111261 1660-11/2I 181142% MIL II*7 IL261 0111ING 16004 46e (No. 1) 53$ (600.11/2) me (1Dp, ..,) LEI Rays-111.. 2611ond 261. FAF to MAP 45 NM liter unusable borsod 15* south of sours* Knees 6090 120ISOISO Asin,S.c4:303.002.151 48130 ARLIN FIVE ARRIVAL(ARLIN.ARLIN5) PHOENIX, ARIZONA 33'26'N-1124)1'W MINK ARIZONA EBCRWY 26L PHOENIXSKY HARBOR INTL (PHX)

FIGURE3.-Arlin Five Arrival/LOC BC RWY 26L. 175 17)6 V- POWER PLANT VISUAL RWY 26L AL-322(FAA) -vmagg PHOENIX, ARIZONA AROMA

limo Ms 6 PNOENOISLYIWRIORINTL EPIE6 3E U1C-7 1132 8 S4 33'26'10"N 112'00'32"W MOM on * saw of MM SO. 101 lOOLL. JET A OX 1. 2. 3, I TPA-See Normals NM, 64 SRP1350. LRA CFR Mae E MN r 4000(Roconononded Ninudo) MU H11001X150 (MPH-GRID) I. I 00.-4/01 - sass W..MP NM=II 5-30. D.170. OT-2110. 001420 MIK IMO 10... Complete boss Iso WOW REL. WRIN413-0A 3.0TCH 55'. &Odin, wen at ar above CAMELBACX 2704 MT ak RD- '0310413-0A 3.0'TCH 60'. Pole Rat tic IMO Foe arressam 1110300R150 (ASPH4i11VD) MOUNTAIN 4 S30. 0.200, OT-400, 001.620 HIRL ARIZONA '44 INIIIL MAWR. IGO Re. IMTMORE 1111T XL: REL. VNI101114-Upper GA 3.25'TCH 90'. Lam GA 3 VTCH S3'Mews 11111118110111111 Altadad medium* Twining by *AI turbaist sett prohibitedswept PPR WA-2132(1000) ist selt sod mishatis GE; 2632(1500) May sett and turbaha. Unitas othindby ATC ell Sabine adt end sett 11500110dear miser at sr Men3000' MILuntil eshillshid on Md. Fly bass lag at least 5 mi lain arpt. Omni* poling tesFelled(Shiba; bomi clubs and carltan maw pindmins aircraft Teaks, A-4, II-4. Vortical (Widow, Hawk, $4 bolted is 01000 On Ray 0114204 pass wslOit 1x41 0410.10430,000 pounds, 001030140 340,000 and Anglo: mum% 14011 - 1430.000 punk, Praia up Is EOM 620.000 pounds, VASI Ray 2111:123. 001040431000 pounds 0410-30/40 540,000 pswale. 1.1011.1 430.000 pound' moll* operateen nry Rwy 0811441 moss weight Ihni 0410.10 MO.= Nowdo. D410.30/40 54,000 pounds, I:1011.1430,000 pounds. FRO Nolification Swim 1.! (MMUS) aE 11111111MIM=MI I&. 1545af 02111111111111111184111/1101111. 121.2(6ar)2444963 611100 124.3 MEM 122.95 MOO MI101111116 (RC) LC 257-9792 NOT FILE PIM ...... TEMPSWISE poyll 1181121612!2(MILICO n r3M 0190M110111 1218 (29V-3W) 124.9 (053' -14V ) 124 1 (147.-2510 MARICOPA PLANT Maw 5500') 123 7 (147'-250* sseoraid MOW 120.7 (310*-062' 5500' and bstow)119.2 (310*-052' above 5500') Intercom And oast of IMO 1117 (Roy 011.411M, 120.9 (Roy 01R2411.) MOM 121.9. 121E15 AURA 118.1 Power Plow at or AIM ele /PPM RADAR REQUIRED 1 above mr. 81111MISM11611111111 NOTIM FIE PIM. weardwr Miaow= 4000 Not cans Pt 111111111110KIRC 115.8SIMChan 10333.25'53"M 111'53'17'W end 0 rah vilbaSy 2555 3 NM to M. Room depicted Oro 1105/14E erky providing 111/111 108.3 MR Clan 20 Hwy OOR GS unusable below 121101 LAC badmums towable beyond 20 south at SOUTH bons oast a Pow Mont OHM MOUNTAIN PIM 010047 Compimo base leg Sow log imo at or rho* on ot so* of PL11111.111611CII (E37) 4 PR UTC-7 32'5012"H 109'52'52"W MOM 4000 foot SIP 1.170 3100 4000 (lloconnnondod Mood.) 1111111.1* 291011110 (TURF) ems am ow woo Igo. won um won no sm WO 41r" 1,101: Shah. IV Ile lbld limb) 250' Ricoh AININIIIIIIIIIRAllagsd csnlinuouiv.Nov01.19 seam in rmws condition with osier seeks on first 1000'HE It-170 OLART NOT TO !CUE ant 01111MICARIIMCMF 122.9 111111011TMS(Nc)riiMss cal, del 802-778-0314 PINK ANWAR owMAN")

POWER PLANT VISUAL RWY 26L PICIOOTT NO (PLC) ea Erma A Law FM. 122.4 122.2.1102-7710314 RIM 1-1I When visual approaches to Runway 26L are inprogress, clearances will be 4 given utilizing in port the following phraseology: wmms

'(I DENT) CLEARED FOR A POWER PLANT VISUAL RUNWAY261. APPROACH.'

WER PLANT VISUAL RWY 26L MINK MUM 33." 113."PHOENIX SKY MANOR INTL (PIIX

FIGURE 4.-Power Plant Visual RWY 26L. kg,

181

FIGURE5A.IFR En Route High Altitude Chart Segment. Appendix 3

ANATITTio IUit IIIMMielf Or TavaliveRfarica usSTAIRS rocour 1110111WamaTemAIMPIPPATM (FM USE ONLY) 0 PILOT BRIEFING 0 VNII maul MOW PLAN 0 STOPOVER

2 3 mussurss 4 mug 5 01PAATuAl POW 6OVAATuRE Put 7MONO 1 Ivre ilNenTloN milluDI Inman at ACTUAL LT? -420.431kBEItOVA13311/4 li".1- FL aa e NTS III Min fve-fves.asu VIA J Idol/ TIN VIA TFN. DO IA CA-LAY.

9 01111TINATION pre 0 Musa 10 ssTM &MOM 11 ammo NOINTL woura Verona us Amacur 12 nu ON luso iswows mapcorra 14 Pkorstaw Awns s Inmate MAMA AAACRAPTtCTAI mu NOM tram LSNWIID

tiAtyDISTranakCONTACTMLIP10W100100,041 / r

CC:WOWAITIONOT ICIVIL MOW? PILOTS. FAR Pan el Auoins you OW on ON wow pen to omega under inanorant bed MS in ', SOTArollel glom folkso Is OM could moult in A oATIpenallynot lo ems" $1.0:0 Tor ouliWeloloon lischonKO of is IPell" ATINIMACI el Ma al weird.* MO AT A MINIM Or moommordo0 au gor. oporoboo patios. limbo 1 P.M TorfolyArenorAi00nOOMire DWI% Night ions FM Form Mal esm CLOSE VFR FLIGHT PLAN WITH FSS ON ARRIVAL FLIGHT LOG

CHECK POINTS ROUTE MACH WIND SPEED-KTS DIST TIME FUEL

FROM TO ALTITUDE NO TEMP TAS GS NM LEG TOT LEG TOT LEVEL TUS2.CAN * TUS 73 :25 OFF CLIMB 350 LEVEL TUS2.GBN 280/46 OFF GBN FL220 ISA -3 INT J104 280/46 GBN J104 FL220 ISA -3 INT J104 280/46 PKE J104 FL220 ISb-3 J104 280/46 PKE TNP FL 2 7.0 ISA -3 START J104 280/46 TNP DESCENT FL220 ISA -3

START DOWNE2 LAX 52 :18 170 DESCENT ( DESCENT D APPROACH

OTHER DATA: *Includes fuel for taxi. FLIGHT SUMMARY TIME FUEL NOTE: Use 676 PPHtotal fuel flow from level EN ROUTE off to start descent. RESERVE Use 726PPHfuel flow for reserve -- 120MISSED APPR. requirements. TOTAL

FIGURE6.Flight Plan/Flight Log. k-

7 183 IKTUS2.TUS)8732S 1 kT:2. TUS) TUCSON TUCSON INTL TUCSON TWO DEPARTURE (PILOT NAV) WCSON.ANTOINTLNA CSON TWO DEPARTURE (PILOT NAV) MOON. ANTONA CINC ' A 11(....s 261.2 ATM 123.8 330.1 NOTE: Rwys 3, 111/1, 21. 291/8 DEPARTURE ROUTE DESCRIPTION require a ming of 4000 (Continued) SAIS RPM* feet and 3 miles visibility 115.4 SOPM1,, or standard with minimum SAN SIMON TRANSITION (TUS2.SSO): Via TUS R .038 and SSO R-261 to SSO VORTAC. Chen 103 dim!) of 250 fl per MM to 65.10 ft. COCHISE TRANSITION (TUS2.CIE): Via TUS R-107 and CIE R-245 to GE VORTAC. NOTE: (Ma Send trandtion requires a TOTEC TRANSITION (TUSZTOTEC): Via TUS R-308 to TOTEC INT. minimum dint of 250 ft per NM to 9000 Net. GILA BEND TRANSITION (TUS2.G1514): Via TUS R-280 and GIN R-109 to CAN VORTAC. NOTE: San Simon tramition requires IlL7PANDirpis Chen 95 a minimum climb of 380 ft per mmto 11,000 feet. NOTE: CIME Required -... 4910 ARIZONA kbP2----tk\WI 1 119.4Y TUCSON INTI. (WS)6 S UTC-7 32'05'51eN 11056'2" FIMMIR i!1\ % 2541 5 Se NM 100. 1001L. JET A Olt 1.2.3.4 ACE CFR India D 11111,1.41 Mff 111116 H109114X150 (11-141-PFC) 5180.13200.171.350,001485HOt 0111 up SE PIMMA tory.ov Ma MIT 111 INL5i. Mit*. Amens &Mee. .wm.m.or VrIPIDDYIlle mak watell.)-UppirIM 3.25*Tchi 91'. lam OA3.0*1or50'. AnestIng Onto. 1..... WI 1112x 1012MC75 5111405120,13140, DT220 OAS up SE MA IBA \N* sh,....X 0ADL MIT Mrllk Thiddeplod 2143'. Ral 1k. TMd amlod 1782'. Pots. 1 141.4 OM 1111" RosuaRk.. 'Ad * , dP (67) Lam WrIS-26 11700114150(MIPH4TC) 3.105.13137. OT.230. 001.500 MIRL awn ill 280. WIN TIN &pied $41'. adresd. iarmir-W11 "32.16" (35) w11127.M/ ' MIRItt NEIL. VA01(66411-8A3.4*TCH 50.3'. Tree. Rattle Muting date. (4.11.2 i, MSTRmatmat Ammoorninmustr. Commercial* be and 8811601110. Aei 506165 Ray 11E red to 840in M beet 400'AOL Om 6 sertim tarn. Sadtsad 1002' and northwest 3257' pond dorm kw 111-29R. kw egil 111 -29R sad 03-21 NM dim hove distance maw/Mktg medals. Ray 111.2981134 welaht 6raR 0011310 TUCSON °9 ttr....-065 9.44$ 3158001M. CO11330/40 405000 awl-1011-1 325.000 66.1.1011-100/200 340.0001h. Roy 0321 wan as 114.0 TUS fir waled IMIR 00 -10-10 300.000 Is. 00.1330/40 375.030 66.1.101141310,000 66.1-1011-100/200 315000 (311) Chen 107 MESCA la FRP NoWleellsa NNW (ACCUM ambeN MMLIETILEZE3 413113.641' 11111011111MIAIIIIMIR U.WAS. w11029.09' COONS! 115 I CEP'''. 1101111111111111118M11 123.11(102-741-1177) MON 122.95 Chen 105 MIN 11S (TUM ea arm. 1.0 I14?- 9611.1222 NOTAM tat Wu. N32`02.00. W 101.45.447 111111111111111011 122.4 (TUCSON FM) W. 142 M9/81101111 125.1 (itay 11 0110*-zw)(Nry 29 275'4551118.5 (Ray 11 2115' -NV) (Ray 29 we-274') 1211.5 (1300-07001) 118.3 (0700-1300) MIR 1111.3111.0 MOM 124.4 cumin 125.55 6111115888111111111111 NOTNA FRE Wit/WM de TUCSON FSS NOW Met not to male. 116.011$ Chan 107 32'03'42'11 110'54'51''W301'isNM to fid. 2570/12E. 1101ITPC urnadde050*-011trbeyand 30 NM Woo 10,500' 350'035' beyond 30 NM below 11200' um 2641 IS/11111 1015 hTUSCian 2211wy 111. DEPARTURE ROUTE DESCRIPTION

TAK!-OFF RUNWAYS111./ R, 21,291./R: Fly assigned heading to intercept appropriate transition. Maintain 17,000 foot, or assigned lower altitude. Expect clearance ft) -, filed flight level 10 minutes after departure. -s.":, TAKE-OFF RUNWAY 3: Fly heading OW for vector to k14- 4,..,, ''' NAME TAKE Off MINUNIMS appropriate transition. Maintain 17,000 feet or moonINTL assigned lower altitude. Expect clearance to filed flight : (Se N . Iv" 3. MO, 21, MA. 40004 or standard 41, level 10 minutes after departure. '. .,. N wI6 whims ads of 250' per PM se 11500. NI DEPARTURE FROMM Candy w16 MO or redo umbra or bet left or AIM es (Continued on next page) =ATC drat TIM VOITAC, M Mom (TIN. figh. OA% labowd) Is apart TIM VORTAC at or dorm MCA or CSON TWODEPARTURE(PILOTNAV) MOCK M120110 MIA far ealerad *may. 185 184 rus2.TUS) TUCSON INTI

Rama 7.- Tucson Two Departure (Rot Nay). L,...... , (DOWNE.DOWNE 2) um LOS ANGELES INTERNATIONAL IprNE.DOWNE2) LOS .NGELES INTERNATIONAL LOS MOM S, CAUFOOM DOWNE TWO ARRIVAL ICIS ANIMUS, CAIRO*" WNE TWO ARRIVAL ARRIVAL DESCRIPTION

TWENTYNINE PALMS TRANSITION (TNP.DOWNE2): From over TWENTYNIFIE PALMS VORTAC via TWENTYNINE PALMS 1-254 to PIONE DME, then LOS ANGELES 1-068 to DOWNE INT. Thence.... HECTOR TRANSITION (HEC.DOWNE2): From over HECTOR VORTAC via HECTOR 1-211 and PARADISE 1-030 to CIVET INT, then LOS ANGELES R-068 to DOWNF INT. Thence.... PEACH SPRINGS TRANSITION (POS. DOWNE2): From over PEACH SPRINGS VORTAC via PEACH SPRINGS R-229 and PARADISE R-046 to RUSTT INT, then LOS ANGELES 1-068 to DOWNE INT. Thence...... From DOWNE INT via SMO 1-085 to SMO VOR/DME, then via SMO R-259 to WAKER MIT, expect vector to final approach course. f 2 9 CI g 6 g 1z

IDOWNE TWO ARRIVAL LOSsmours.cAuroess LOS ANGELES INTERNATIONAL DOWNE. DCULIL.IE1) FIGURE 8. Downs Two Arrival (Downe,Downe2). 187 (CAT II) LOS ANGELES INTERNATIONAL MCA LS RWY 25L AL237 (FAA) LOS ANGELES, CAL HELIPORTS LOSANGELES*PPCON 124.5 3111 6 ..../... -E741CtIre P.4/,. LOS ANGELES (Kn. (LAX) 9 SW UTC- 8( -70T) 33.56'33"N 11824'26"W LOS ANGELES TOWEI... ogee..., 126 8 S4 L01 ,1111E0 REL 100, JET A OX 4 LRA CFR Index E N 133 9 239 3 OAF) IRV RE 11601(60 (COW) COMM S 12095 379 j./ 8111, 0-30 MIRL NELMOO 217 ONO CON /r ... --.... P4c---. NA le H63)(63 MONO 5-15 URL IAF "Ea%sr.., N 121 65 327 0 4000 to Down. Int SANTA MONKA AIRFORTIMIAMIR Attended continuously. CAUTION.Turbulence may be deflected upward from the blast fence 5 121.75 3270 111) a smo a .. to A* SU R 3411 75) 1601 east of Rwy 25R. Now sensitive located and LOC ((2 7) arpt Numerous birds on and aNC DEL Chan 45 N in musty of srpt. Flight Notification Wm* 121di327 0 SMOGY INT (ADCUS) avaitiblo. Rwy H2 led on req to USCG. Own.tttedownfoe. Rwy H3 etc twr fortfc pattern AT1S ARR 1331 SMO IS 5 DM M7000 EATIlet IIATAK1NCI8 U.WAS DEP 135 65 AM mommum COMNUN8110118 AM AIMNAL133.8 UMW 135 65 (213)646-2257 / 5000 to &Muds liffail122 55 A 1173 4000 to Down.\I In \ 1161111110111E IN (MR) LC 6441020 NOTAM FILE LAX. /Stringy int 060_------SLI 5.341 (4 7) 4000 to tt6400 to oar (Is I TOWER 120.35 (Helicopters oat) 119 8 (Helicopterswest) ORD CON 121 75 (S comply() 121.65 (N and LOC (2 7) Down* la' saw Mt complex) CUIC DEL 121.4 LIMMA OM/INT 49 (7 3) 249. (2 7) A ILAX ascot . TCA4bsep R See VFR Terminal Area chart LOS ANGELES. Aa59 7 4 DME Hunt, Int 113.6 1900 496 2.11) '"376± ass Cha 249 (4 1 ,... 114,1111111011analit_ ..... -"*"...,...mg.---- FUELR IAF) ILAX I HONDA NT D(owNE 25 DME I-LAX T INT MI 14.AX 2 D M E .0 1 2 . m I-LAX DME 1 \ 1 at ti 4 4000 to Down. Mt L1ZEEWM * 585A ILAX Ibe SU 1.344 (11 2) Chan .'" /and LOC (3 3) \-

LAX23 \\ ___..011111ft! *St'-2 R 251 0 11M "ft...... [Mi 270. RASH...-. IAF LAX 12 DME ....,../ SEAL BEACH -. 115 7 SUHA L-/ ...... ,"... Chan 104

pnxidw. DOWN! MISSED APPROACH MR ELEv 126 Xvri 255 Id0 1112Y Dumb ta 3000ton Mft skating tem 5,,,A NA I-LAX 13 DME 1.1A,2 25 DALE Rwyaidg 99.14' Ie 2000 we 220* hooding Wad HONDA INT, L44ET INT intwimptine LAXR-192, Man dale lux I-LAX I is 2300 to Inidt Mt /LAX 12 DME. ILINIAA12 I DME I 22.310MI 0AvINT I Mar pH 14AX74 DM4.,.. I Kw TCH 36 ON (RA 163) MMitin.'," A215 OA ill) OIL/4 192 NI A% lablalitgleal o., r) . TDZE MIR 4 I 91900 'Awn addliWissd 101 ...... ' 1 ,.,.--,-,.; i zil* Ill I 1 by ATC. ) t % cAnocaw A a c o 'Z' !HIM 251/16 t50 MA ISM P --.-.' SAS 2111 201/12 103 (RA 111) nip TDZE liravissessus ggprogdwn audwinsmi with Runway 241/1. 101

CATEGORY II 0.5-SPECIAL AIRCREW TD1/CL Rwy: 2411and 251 MIL boys 71.251. 71.2* & AIRCRAFT CERTIFICATION REQUIRED 62.211 end 61-211 arsrm - I 11124'W WI AN011111, LS WA' 25L LOS ANGELES INTERNATIONAL(LAX iCAT II) Appendix 3

him /wool 01111(o 11104011

MI STA0110 101101PLIS1 "1111TA AMTNTIATIOTA10111WATICOTICIN (FM USE ONLY) 0 PILOT BRIEFING 0 VNR nnua

1FLIGHT PLAN 0 STOPOVER

1 "Ill 2 1010111111 214.00AFT 1v111/ 4 Mg 5 01011Tullic PO0a 6 DEARTOW nue 7 :Vslo WINTIMATOI MM. 11011001017 MUD 00 a. (.(010111D 1Z1 ACTUAL (Z) miopoema/V//o a 0o 0 Dm os BAKER sWilin Or PUSH! ilk.% 42,6e'C. 1/311 via V394 P6N1 Va#0 LAX

*ranizirm 10 ESTten IMOUTE 11 111".18 4 g11111.411eg lagoL0001130AmoNTL) Afton taw moms111.1*(0141 lauwatn a AinCWTHOMESAX 15 wins NOUN AlriUMB Ammo

DESTINAT100 CONTACT/rolowoort WA17 (OPTIONAL) i 5 $001011011WW1 CIVIL AIRCRAFT MOM. FAR Pert ft mums you lie an le le Nip pionO opines unrest wolnanont Ogle Ma in conireissd Mom FalunID NO could mult Ins DWI penally 101 lo aucemel 11.000 ROM Mx NIAvaletion (Sselion 101 01 be A 0 8 1 0 0 A c t a1111111. as g o n d o l ) Nina de W MNOM Plan 4 mccownencle0 ma pod oposbna (maimSwaim Pei 111 1stvelp.iientenis eeneemog DVF/1 Nighttime. FM Form 72334 s43) CLOSE VFR FLIGHT PLAN WITH FSSON ARRIVAL FLIGHT LOG

CHECK POINTS ROUTE MACH WIND SPEED-KTS DIST. TIME FUEL FROM TO ALTITUDE NO TEMP TAS GS NM LEG TOT LEG TOT 2700 BAKER V394 * CLIMB :10 250 lbs

.. . . , JOIN V394 290/36 V394 DAG 110 15 12,000 ISA -2 ...... DAG V394 290/36 POM 110 12,000 ISA -2

PIRRO V394 290/36 POM 110 INT 12,000 ISA -2 PIRRO INT LAX DESCENT ANDAPPROACH :17 955

* Includes fuel for taxi. OTHER DATA% RIGHT SUMMARY NOTE: Use 1420 PPH total fuel flow from level 'TIME FUEL off at 15 NM from DAG VORTAC to PIRRO INT. EN ROUTE RESERVE Use 1235 PPH total fuel flow forreserve 200MISSED APPR. requiremnts. TOTAL

FIGURE10.Flight Plan/Flight Log.

11 MES LOS1 AMIIi.ESIT VI ROMAWROS -Mh CENTER2302E 00alti NOMA rss OS CENTER/ESS VCV BRUITS RCO CENNN BarstowANGELES CANN 23 13252817 fuu

CAC DAGGETT

113.2

NEC 21.212LUCER NECTINI INS CNN/411

CNNIr. MS

in111-2H MN SW

V131ARIAN1 Wagt Appendix 3

ftmommotomuftmeal mu s ums wawa uarmarm":14=wAnTr (FM USE ONLY) 0 PILOT BRIEFING C VNR orms rUONT PLAN ciSTOPOVER

, me 2 Aliourf 3 maw' mit/ Taus 5 011V/111111 POINT 4 oapaitAMIIMI 7 Lm.umN0 10111MRCATION ancua mummy* mama MI vy os fooposto 03 ACTUAL IA "li / S LJer/ efteArreN FL 310 aineirAtOikn. tue b BPPA L.CI ONE NL VS 7 War 7647-3".511, oele.

Anna 10 on Tao atatovra 1 I ammo %ramorm' mums MUM

PM elSONO 1,11WNW! MI.0117181 gaatorsNahamoms amamma mamaaAmamiKw BM ISPAAOIR HMIS 1111011

NAj7°mimic« CONTACM111.1001410,11000L)

MOROIAMORAFT CIVIL AIRCRAFT PLOT& FAR Pan Al mynas you OM an IFR NW Oen lo web oral innument NO Mum In cenlialel slapaon Foam Is as Null ma Ina WI wen as, io owed KM kw ugh dokilon gaoler 101 of VII Wag Animism/WI WINS. onamends4 Fling ale FM 111.1000 Is skonvonnad sea goalopsnins padiss. Su Woo Pon IR ler onielonwe sonsunn. DVITI alpiplans.

PM Form 7233-1 pia CLOSE VFR FLIGHT PLAN WITH FSS ON ARRIVAL FLIGHT LOG

CHECK POINTS I ROUTE MACH WIND SPEED-KTSDIST TIME FUEL

FROM TO ALTITUDE NO TEMP TAS GS NM LEG TOT LEG TOT LEVEL * BUF 70 :14 2900 lbs OFF CLIMB .. LEVEL HL547 300/46 YXU OAF FL310 ISA +3

INT HL547 300/46 YXV J547 FL110 ISA +3

INT .1547 300/46 J547 **ECK FL310 ISA +3

*g/ART .1547547 280/42 ECK DESCENT FL310 ISA +2

DESCENTANDAPPROACH 30 :16 650

. .

OTHERDATA: * Includes fule for taxi. FLIGHT SUMMARY NOTE: Use 8,650 PPH total fuel flow how * TIME FUEL level off to start descent. EN ROUTE Use 7,020 PPH total fuel flow for RESERVE reserve requirements. -----.1.3V-41SSED"PR ** Variation 7W TOTAL *** Variation 3W

FIGURE 12. FlightPlan/Flight Log.

193 13 &OFF AID/GREATER BUFFALO INTL UFFALO ONE DEPARTURE (VECTOR) BUFFALO, NEW YORK NEW TOM A113133.35 CNC Ott 101"010..... BUFFALO 134.7 1.11.5MEI-v:1 BUFFALO AIRFIELD (900) 6.1 SE UTC-5(-40T) ONO tai Chun 92 42'51'40"N 78'43'00"W OETROT 6706 S2 PIM SO, 100U. 121 EP 237.6 H4336 13' LAN w7e40 li IMMO memo (ASPH)54 AWL 'UMW TOWER - Mp 120 3 2371 L.12,14.3 SYRACUSE MOW Trees. R128 Tree 117 0 SYR Pa r - %MORT WWI& Attended deyloght hours. CAUTION. Ultralcht activity ROCHESTER Chon 117 on aro Airport ists opr dusk.0700Zt For Ilooacc Ilf-14: N43.0963 'moray lilts after 070025 Owns 7164684901 BUFFALO Chan 37 W76°12 30 CONIMNICAMINt CTAFIWCON 122.1 LONDON_ 116 4 BUFinfi: N43°07 24 L 12 25 26 EI 3 6 IMO PIS WM LC 631-9630. NOTAM FILE BUF Chen 111 W7740 43 117 2 YXU MIT..." ® rmastnaveza1231 Chtn 11-9- N475574' 1. 12 25 El 3 6 N43.02 28' W7r38 40' PAW AIN TONMINIMat NOTAM FILE BUF L 12 H 3.6 W81.08 92' %VFW ft =MC 116 4 BUF Chan 111 42'55'44"N 78'38'46"W 225'4 9 NM to fld. 730/08W.

GENESE0 GREATER BUFFALO INTL (BUF) 5.2 E UTC-5(-40T) 42'56'26"N 78'43'57"W 811104f 108 2 GEE r 724 B S4 MIL 1000, JET A OX 1. 2. 3, 4 LRA Chan 19 CFR index D WC. O, WM X IM1618 H6102X150 (ASPH-GRVD) S-75, D-195, DT -450 HIM. CL N42°50 06 0.6% up NE VP W77.43 98' 1W el: WAR. TDZ. Thid doled 335'. Pole. SSALR. DUNKIRK 1 12 25 , El 3 6 WV 1448 H5376X150(ASPH) 3.75, D-100, DT -160 WM. 0.3% up SE. 116 2 DKK Elk WY AYIAIR Chan 109 VAST V4L)-0A 3.0TCH 55'. Tree. RWf M ROL VASI(V4L) -GA 3.0*TCH 55'. Fence. 114 7 YOO =me N42'29 43 NIPORT SWAM Attended contInuoaly. Landing fee. CAUTION-Jet engine toot god locatedappoximetWY 3600' iChimes, W79'1646 from apnoea end Ray 321400' south center line. Jet wheat may mach altitude 100' ML. Opt conducted N42 42 40' L 12.23, H 3 6 WELLSVILLE W6053.28' tll 4E11 acceeionelly 1300230002. CAUTION: Numerous types of birds may be encountered In holdk* patternover Grand L-12.23.11.3 Cl,,,, 51 Wend up to 5000'. limy concentration of Gunk, Illeckelres. and Stsr5miup to 5000' on and m vicinity CI Mt. N42'05 38 Ow on and la vicinity of amt. Wit Notificabon Service (ADCJS) W77°59 99 DATA MINI& U.WAS. L 12 25 H 3 6 owe CONWINICAININ8 All 135.35 511111:011 122.95 114JAMEST. 7 1HW ligiW"' VC STONY FORK IMML11111 OW) en opt. 122.6 122.2 122.1R 116.4T IX. NOTAM FILE BUF. NC41An19341 112055FF,w,;%s IMPFOLOMP ergo 1231 (055*-1941 126.5 (195.479.) 126 15 (290*-054.) W79.07 29' Chc. 76" IIMOTOVIII 120.5 SWOON 121.9 L12 23, H.3 6 PDC* 124.7 PRITAIICUIC 124.7 W77.25 21 AIM etc MP CON L 25, H 3 6 7 IMMO AIN TO WM** NOTAM FILE KO. DRYER 113 6 D111041 BRADFORD IAIMPLOWVOMAC 116.4 BUF Chen 111 4255'4ANN 7A`311'411HW 288'3.5 NM to lid. 730/08W. Chpn 83 1166 In ra,14: SLATE RUN ameemaae 231Bu43'00101"N 78'39'04"W 233.4.4 NM to lid. N41.21 48' Ch n113 113 9 St!:..... RAU mop 204 1311 42'52126"N 7849100"W 053" 41 NM to fld. W12.0973' N41 47 1131 Chore TO L 23, 143 W71137 1' N4130 76 111.314UF ftwy 23 LOW KLUMP NOB. Inner marker out of so Indefinitely. Back course unusablebeyond L 12 23, H 6 w77'5822 15 NM. NOTE Chan not *a Hole L 24 25, H 3.6 Ra 108.51.01 Rwy 05 LOM RAll NOB. AM ELEV 724 DEPARTURE ROUTE DESCRIPTION All aircraft cleared as filed. Expect vectors to filed route or depicted fix. tAdintain 10,000' or assigned lower g altitude. Expeict further clearance to requested ..# altitude/flight level ten minutes after departure. All Runways: Maintain runway heading for vectors.

..,

.7 195 :UFFALO ONE DEPARTURE (VECTOR) BUFFALO, NEW YORE BUFFALO /GREATER BUFFALO INTO

FIGURE 13.-Buffalo One Departure (Vector)- Buffalo/Greater Buffalo Intl. Oiellot Pea COMmunitv 114.0 ICE NorroarWY onUN

zp 277 1

St Clow CoIntl

09 \1°* flu nrtroRokton34W.,0 O L1i Kersch mun,

Ellik,,, 500 is

SOUTHERN C oronto I.,,.,

Hamilton St Clow Co Intl St Co OINESE0 101.2 GEE (I)

AIYMEW 276 WOO IN

willow Ru

aigmmiimm

Flom 14.FR En Route High Altitude Chart Segment. 196 197 ti

Penn rme MAIM MORI IOL 011FARIMINT Cr/11A111,011tATION T* StARTIO alseaxin ramematrawasAorwarmaicat (FM USE ONLY) 0 PILOT BRIEFING D VNR IIIITYLO FLIGHT PLAN 0 STOPOVER

1 Imil 2 Arnow 3ofICOAFT TM 4 me 5 6 overnume mie 7 rim foorrcrenoN 'POCKMUIPM MINOPEW of 0 Wip3StiVisa At/60.MIDWAY Milio 48 ROM OF Flee CANALlIKEE 1146 5814 Inv CRS 1186,411.376ygu 1110r11 191i BAC 9 ioEST TS* IIOUE 11 MAURO PAILFALa 12 ' ON WAND IrlianOMTE allfanTtel 611 'kart moo A0011E514 MEMO& MAMA I ANCIVOT non SAN wows* Ion NM* ABOARD

NAj7CaTNATiON CONTACT/TELEMONE 401MONAL)

WOMAN OF AMORAFT CIVIL AIRCRAFT PILOTS. FAR Pea In inquino you Ni an OR Ingo pin N cow*under ineOunont Sant rugs in vordloRIFS iliflaiRio his* to No could null m CNN Wally on N am* 51.000 * awn **ion (Sadao OM of no Fads* MVO* AO of Reg, al onencOS iienedaVFel Mold pion is roconvoonatima good Opaline onictioo 80114110 Pin es at mulrentenle cannoning OVFR %owes

FM Form 7233-1 (MI CLOSE VFR FLIGHT PLAN WITH FSS ON ARRIVAL FLIGHT LOG

CHECK POINTS ROUTE WIND SPEED-KTS DIST TIME FUEL VAR FROM TO ALTITUDE TEMP TAS GS NM LEG TOT LEG TOT CANAL LEVEL * THREE OFF CLIMB :18 105 lb. LEVEL J146 260/45 SBN 1W 160 FL180 ISA 48

J554 260/45 SBN CRL 3W 160 FL180 ISA . J586/HL586 285 43 CRL YXU FL180 6W ISA 160 START I YXU KL547/J547 285/43 DESCENT 8W 160

DESCENTANCAPPROACH 80 :24 85 ,

. ' C OTHER OATH= * Includes fuel for taxi. p__BIGHTSUMMARY NOTE: Use 146 PPH fuel flow for -TIME FUEL fi cruise. EN ROUTE Use 136 PPH fuel flow for reserve RESERVE requirements. -- 36MISSED APPR. TOTAL

FIGURE15.Flight Plan/Flight Log.

198 16 Appendix 3

11014 CHICAGO MIDWAY CANAL THREE DEPARTURE (VECTOR) CHICAGO, ILLINOIS ADS 120.03 MIDWAY CINC DEL 121.13 MIDWAY OND CON 121.7 MIDWAY TOWER 111.7 226.3 MIDWAY DEP CON 111.4 311.0

,,/ 17 .... IIINCK 49.48' W11'40 33'

CHICAGO HEIGHTS 114 2 CGTEM JOLIET Chan 89 112 3 Jorens- N4130 60'-W8734 27' Chan 1-23, H-3 N41432.711'-~19.10' L-23, H-3

ALL 1FR deprtures are radar vectored to the first enroute fix, and provided headings that give obstruction doaance.

NOTE: Cheri net se mete DEPARTURE ROUTE DESCRIPTION Aircraft departing Runways 13l, 13R, 221., 221, 311., 311, climb to 130w-before turning east. Runways A, 4R de re climb to 2400' on hooding 090° before turning non . WMa 'NNE4 DME of MIDWAY. Maintain 2000' until 6 DME from MIDWAY than maintain 3000'. Expect clearance to raquostod altitude/flight level 25 DME from MIDWAY.

SININIPPAJIME..4 1-096, Thence... DEPAIITURESj_ _Maintain 2000' CGT It-311, then maintain 3000'. Expect clearance to reauostod altitude/flight level crossing the CGT R -274 or the JOT R-314. bIAMPO DEPASIUM Maintain 2000' until crossing mull-34A Swim maintain MOO'. Exped clearance to requestad altitude /flight level crossing the CGT R-011.

CANAL THREE DEPARTURE (VECTOR)

FIGURE 16.Canal Three Departure (Vector)- Chicago Midway.

199 17 6. INIFFALOAVIATER @UMW I. (SUFI MATER IMFFAIA INT1(5UF) 5 E UTC-5(-401) VNAVRWY 32 42'56'25'N 754317"4 51311611 oUPPAID. WM 724 S $4 NM 100U.. JET AOX 1.2, 3.4 tRA AM! kids 0 (14.41.1,42R IUMAID Mt CCM 11106543 141022150 (42141-000) 5-73, D-195. DT-450 10111.(3. 01% up NE 1231 MU IMO UNA TOL Thld &pled 335' Pale. WM MAUI. TOL UMW TOWN 2111411 1153751150 (ASPIO S.75, 0.100, DT -160 MIRE 0.3% up SE 1203 11/74 ME It W41041)-0A 3.0' TCH SS' Tree Wf M NEIL VASRVI1)-13A 3.04Tal 55'. Fence CND CON arenewas Mended centMume% landing M. CAUTION -Jot engine MM Mindlocated eProllhatelf 3600' 121 WI how appreedi and May 321400' south mast kne CUIC OM . Jet otont am teach UMW 100' AM. Opo amductsd --1 124.7 WI aceselerelly 13032300M CAUTION Numerous Nees el beds may be ancaunletedin holding whew war Grind 1$49 4100.6'N 7r53 rw AIR Wand oft M 5001. Now C011iellii10111 of Gulls. Illwidirde and Methylod to 5000' mind eh *INV 4I opt .7 114.4 SUF 302.1-22 2 AT* Owe an and in Molnily h apt. Might Notification Service CROCUS) welleble. 730 UM31 111411111141111111 LLWAS. MMIIIMMINIR NM 135.35 MOON 12E25 4236.3'N 78'43.6'w _ moon* 0111,) an opt. 122.5 122.2 122.1R 115.4T OL NOTMA FILE SUF. 116.4 51471006 fl- 3.5 211114414144/MR 1233 (0554.1414) 1263 (195*-279') 12615 (210'054') A 1010.11411111 1203 MOM 121.5 130 A Well 134.7 INIUMEME 124.7 1054 A 335 MN *MO 0111 MRS MISTORAIMMINE NOT* FLEW. onoft551500116.4rawawn 111 4es5'44.14 7r3r4rw 2114433 NM M fit 730/0N 111211,1114011111 231 11U 4300'01N 71139'01'W 233.4.4 NM 10 fid. unusable beyond 12 NM MEM AM 314OS 42521rA n'sVorw osr 4 5 NM lo fld. V 111.3 aaur Ray 23 Lou war 2505 kw* ntatMt eiA at wc IMMO ots.5.0cam wombs Woad 15 NIA. 42'5E314 7r3e.vw WALES U 1011.5 HAIR" 03 LOM MAll NOIL 116.4 URN 175.1- 2.5 42'45 1N Mt 1W MI 710 1164 hue 141040.0 111 730

3152356 An 400 (044,.....6 00) 04151 A2314

UM A

WALES SIN 7241 Ilw7 S Me Mr wIlT MUM 01100A01 cwo. 3200 Clhob M 2700 aweGres WPT WPT ww hat S

MAPWPT 6 2,1110 `12,0,, 4P.N' 4, / 744 . .,- . S .4 tol 750 \ -Ls pg.-4.LS MI ',.. / 714 CATEGORY A 1 11 0 11111-1-4/- / '''P 542 1220-1 300 i3600 122011/2 an wpm) /,4 UMW%) 1220-1 on (!00 5) 12204 1/2I 12110-2 pus / 191(500,22)ISSA ME04) A . ,.., 313'» 04 MAPWIN

MIL Ruh 32 TO2/C1, Reps Sand 22 MN Ruh 1442 NM Rue 343 201 RNAV RWY 32 42°104- 7544V IM M0, NEW Ms ataaraoMarda SEPAID ea Min

FIGURE 17.-RNAV RWY 32 and Excerpt (BUF). ndlx 3

r.:so A 0 '4, 1.

itl I

i/ ..1 220

OA 0 MO' 6 NM

CV/ MINI `-ese4,0 14's ik 0 clirr 1- I

, 4,4444 .L.L.LJ-1°_, ifIr_____. --I INN Y 4,4 v v 1 1141004 DENSITY OF HELICOPTER AND le 'If MID WINO RAMC OFIRA ON THE HUDSON AND V 4*4 EAST RIVER TCA In AU AIRCRAFT SEIB $. IN IDE ANNOUNCE ON 121.075 THE EAST RIVER AND Ts _MTH /CA IUDS FOR TFIE MORON mil. I +...211.MALMIISI . e a -a- -1..---19-1imun WILL ....

FIGURE 18. Helicopter Route Chart. No Aiwa* OW Ma MUM 1114 MATO 111101411, iliertas""Prjo=linal6r6 (FM USE ONLY) 0 PILOT BRIEFING ovtga menu PLIOHT PLAN 0 STOPOVER

, 1 we2 mow 3MOW MN 4 nu TsDIPMTuld PONT $ opanns. TUN 7 rim moniwcason anew mown ammo MP POMP= la AC1104 14 "N 10MIIIIE IG/AARS DPW fic, 640 WPM NTS OFW 11541 SILIE.CUGAR IA N zszrompr'10 or us mono 11matima wows Nouns eI TA a jas owejrnAMPINAIAMMO, 14Awn mks. moms. IMIPHOPE NUMMI AMOS, MOMSAN NOM OPIUM

MA7701111TraisON CONTACUMIPHOM farramom

mammaANCIVOT CM AIRCRAFT PILOTS. FAR FM IR NW/a pt. Os on IMO., P. %awes way minoseesosmks In seAksilse Mom Foam% Ile mai mistAI la a sITAIweft mots mom 111 /10 ler fah %/lobelia 011COln 101 st OM FaikralAvkillenAme/maseftsidee FINAIMIAWRIIIIIMIRIARANFRNARWAIINIAssmoweavonesse.seerso Pot SIMIMMIIMMIIS teneliningDKR NOOrs FAA Form 7293-1 04R) CLOSE VFR FLIGHT PLAN WITH FSS ON ARRIVAL FLIGHT LOG

_ .. CHECK POINTS ROUTE MACH WIND SPEED-KTS DIST TIME FUEL

FROM TO ALTITUDE NO TEMP TAS GS NM LEG TOT LEG TOT

LEVEL * DFW 27 :10 125 lb. OFF CLIMB , LEVEL CUGAR -01EL_--- 225/36 OFF 15,000 ISA 248 I- START CUGAR4 225/36 CUGAR4 DESCENT 248 12 15,000 ISA

DESCENTANDAPPROACH :12 130

1 . , , . 4

OTHER DATA: * Includes fuel for taxi. MARY NOTE: Use 650 PPH total fuel flow form level TIME FUEL off to descent. ENROUTE RESERVE -- 85 Use 712 PPH total fuel flow for TOTAL reserve requirements.

FIGURE 19.Flight Plan/Flight Log.

203 2° Appendix 3

13 11 W01014 s Slue Ridge

,1 134 15 377 1 IDenton Mono InrtruvIrI MPUI 6421. 50

340 32 SA Ak

(KassNonh)Alia*401) \$1 707 30 (14orNwroot llogionol) 0 643 33

ANNA 33'00 0 FONT WORTH Cam) ao c Koller TTTTTT TTTT NAMMIA NSP."."31 a°846281" p Wall 1240 317.4

(130.4.) 673 31 A-` O A. A.

Delleo-Ft Worth ing 603 114 ATE AM 117.0134.9 DIP 133.3 URI o (M Hollargoor) h1 o FM Weal Moodrom ... 114114: OlAtiChaffrlaiN e ... *0 A 710175 asu ,,18 A4, ATIS*120.7 t V V INIFIL p CAIRN WAS- 119 41/ 0,VS' #40,1. lf' F1 MITI 1, 1 1 Mt IA Ali.4 es, au 117 / p.111 gi491LNO/ ASIVP A4 ATS11271110 Orond Prairie Muni I NAVY KAWO 1 543 l 40 0 Cleo alli llodhini

8 136.5334 . 0 Aril ( .,, 0 Arlington Muse0 301. 40

Kgeonero Strip) 740 L 39 (lucki 725 1 35 *(OokGrove) 6901. 34 a 40R CONTIN01.111

KEINE MTV

KIWI swam Muir

Nee

FIGURE 20.IFR Area Chart Segment

21 204 FIGURE 21.-1FR En Route Low Altitude Chart Segment.

205 22

OR/DME RWY 32R A14461 PAN la3US INTIMPTININTAL UGAR FOUR ARRIVALCUGAR.CUGAR4) HOUSTON. TEXAS 1631.161011._ HOUSTON AP CON 124.3$ 237.7 004112 HouvaN on CON 114104r...... 127.25 370.1 14..."Y144!AST HOUSTON NTERCONININFAL MU IAN 2$ DALE 124.35 MI MST 114.03 HOUSTON TOWER 112.1 277.7 NAVASOTA ONO CON 1131 INV / 121.7 Chem 101 CINC OEi 1.24$ 112.1 ARS 124.05

pAPI a

CUGAR WOr1S.,Y 010.111s. w1610.67 Wer0.11ITURS0Jdas Nowa( TION bowl deonnos Is ages et 10000'. OAdS Turbots,. ma of 2302 LAS. IAN 43 DME

3000 NONTOONNY 45 COUNT.'

lEPOt AN IAN 10 DME ft-opi r- DASSIT MACED MDA1Ia% . NAVASOTA I142P IMP TNT, WHIM .62' Chon DAV° WAYNE 0-2113 HOOKS MEN

N30.01.717 W.00.

NOTE: Own not N scull

KEE TRANSITION (BILEE.CUGAR4): From BILEE INT via TNV R-334 and IAH R-305 fa CUGAR INT. Thence ... . COLLEGE STATION TRANSITION (CLL.CUGAR4): From CLL VORTAC via CLL R -100 to CUGAR NT. Thence .. . . JUNCTION TRANSITION (JCT.CUGAR4): From JCT VORTAC via JCT R-081 and 460/24 30 (4004t) CLL R-263 to CU. VORTAC. Thence CLL It-100 to CUGAR INT. Thence .... LEONA TRANSITION (1.0A.CUGAR4): From over LOA VORTAC via LOA R -174 to CUGAR INT. Thence .... From CUGAR INT via IAH 1-305 to BANTY INT. Expect vectors to final approach course.

207 CUGAR FOUR ARRIVAL (CUGAR.CUGAR4) HOUSTON, TIFJCAS VOR/DME RWY 32R WO11111=1.

FP3URE 23.Cugar Four Arrival (CugKCugar4)/VOR/DME RWY 32R (IAH). Appendix 3

maze arm. Nom Astovit OW Ns MUMS la Ole Miliert OF IMMISPORTATON MI MAUD iliaOLOT NW" MIAMI AOMINIFINTION (FM USE ONLY) 0 PILOT BRIEFING 0 VNR iirrv..1 PLIGHT 0 STOPOVER

Urn 2 *MOW 2 Aelpilin Mir 4 mug 5 Ovolnuot root SOPMITuIE TOR 7 :woe nowitimom- swift souptopri- Ammo ~ONO a) ACTUALiso OOP&5/13044lambFil ), SOa 510515110P *VOW oPM V361 sait.Cild-Altq SAW ID mitor"ice...."I 10 eVme swami 11 mono

Hors Od a RIK CM SONO ,1343WINAIPPPORTM grtorsNow Pawls a Memo.* mum a otoclorr mcom. soK Iraukoto Woo 11111111111111

NA 17OUTMATCHCtorrACTfilltiMONE (OTIONAL,

6001011C0WPM Cool. softepon malt FAN Pad III noulles you me an Ira Ilipil Oen ft open% war inalrualsra loomnil= th senkeled MINNSFalun Is So could Mull in a eMI WWI, not 5o acme $1.000 tor ugh 4olollon Illoollon 001 of N. Podsnal &Woo Aosta MI mamma. ging ea VIM INiNtOn iswoommooleil as a poll oporatino plooliooIWO* pol OD los wouloonom conoornloo MOM Nolo pm

FM Form7233-1 (1141) CLOSE VFR FLIGHT PLAN WITH FSS ON ARRIVAL i FLIGHT LOG

_.,

CHECK POINTS ROUTE MACH WIND SPEED-KTSDIST TIME FUEL

FROM TO ALTITUDE NO TEMP TAS CS NM LEG TOT LEG TOT LEVEL DFW 23 :14 OFF CLIMB * 23 lb LEVEL V369 225/36 OFF CUGAR . 15,000 ISA 115 , - CUGAR4 225 36 CUGAR4 START DESCENT 15,000 ISA 115 37 si DESCENTand APPROACH :16 17

OTHER DATA:*Includes fuel for taxi. FLGMT SUMMARY * TIME FUEL NOTE: Use 65 PPM total fuel flow from level EN ROUTE off to descent. RESERVE Use 72 PPH total fuel flow foi reserve -- 12MISSED APPR. requirements. TOTAL

FIGURE 24.-Flight Plan/Flight Log. Nip l WW

COPIER VOR/DME 117°AL 40S7IPAI4 LOUISIANA NiW APP CON 110.0 224, IKAISA DDwdll * NOUNIA-TEMEIONNE (HUM)3 3EUTC- 6( -5DT) 29'34'03"11 90'39137"3 311111186111 11Ik1 IMMO 9334 ON CON NIL 100, 10011. JET A OX 1, 4 7PA(3ao Remits) Ilk L411 1211 661113E H50012200 (COM)2.50, 040, 07.137 1MRL UNICOMInge IR 1* MAU3R. VA313411713-0A 3.0TCH 52'. Trot. we*NEL N311(4404-41,4 3.0'TCH 39'. myna1149911200 (CONC) S.50, 0.70, 07.137MIK MIN 1! REL. VAS(NSTD)(1A 3.0.CH 34'. Rood. MN* VAIII(Va)-4313.01124 39'. /111141171111111111* Alterakolderon4u0k.CAUTION: aids on and in wicinity of amt. Oxygen avb1 by prior muse 594.6760534. ?CHYME MIK Ray 12-30 and Ray 18-35 and MALSP Rob 18 and REIL Rwy 12 and Hob 0411 36 CTAF. TPA-1009'(1000'), WOW pound 1509'(1500'). Control Zeno offortivo 1209033028amid. 140924001$ 313 and inn. 11131111MSATA08111362 (AVMS 004) 3794309. ammumaineaw125.3 ATM 12025 MAIM 122.95 K 111111111111111 (MUM fret ed, del 1-11934/8-111t1EF. NOTAM FDE HUM. TN M* 122.13 112.07 (DE MOOD F3S) 1111131113116118/811114111 1139 Ma 125.3 113.35 (12090300n Mon-Fri, 14002400n **Sun) ONO CON 121.3 11/3114MNI6NANIAIMIR NOTAM FILE DM. 111311)11111116 112.0TOO Chin 57 29'39'51"N 90'49'44** 117'10.2 NM to fld. 10/05E mom219 HU 29'39147"N 90'39'34"6/ 175'5.3 NM to fid. NOTAM FILE HUM. 13 1011.51441)11 RWT 11ILOM HOUMA NOS.

AIM ARMAGH no no Cloth le 1000 An TOD S OW 0 DIM 1.110o, lows 0#111 CAW and loid. ITMh.. 1 1 .,'1 1 1 evemlineum ggs 1 1110 NA 1 10.2 WI I I I lo--- Inn +122 CM/10097 cone

10117 44044 40(!00M NA

1141440 MOM MIMI dead: 1. OM& Mai nikkosfor on UNICOM; when nee ovolobio ea 244w 0Aoons WorooRonol Walonni P104)ehlonsior toolno 'ad income MCA 1401.0. 2. A CTIVAll AWN Roy MK Roy. 1$42 or 1240, Roy 12{TAt

COPIER VOR/DME 117° 2 r3414413.4" 211

FIGURE25.Copter VOR/DME 117' (HUM) and Excerpt from A/FD. Sarni EAKE TANOE/LAKE TAHOE tbA/DME-2RWY 18 *11416 (FAA) SOUTH IIIIIE TAME. A ME GAM. WEIR 171111 NUM LAKE TAHOE filla PIL1 MUSTMIII... TMEGII EMIR* 9220 1171 MO EN. IMUIR* (TVL)3541 UTC-11-7171)31.531rN 119.5V40''W 1111011111111121 IS 1 MIA PO) 227.11 Chen 1 1114IS4 NW lOOLL. JET A OX 3 TPA--See bawls CR Index El 1141.1.411.1A ONO CON MN= MO MAMA 1116441(150 (MPH-WM) S71), D.125, DT -210 111.11 11 DIVA 12000 MIT 19 UMW. VAIN(S21) -0A 3.0'10147' (data only). Tree. WO= 177.14 -11617 201(NI) 12000 MU Wt. TAM ddial 2037'. Tress. tk. 201' (2.3) MIMI IMMO Mierded centimenly. CAUTION-Own *alb met/ be encounbinid dose to the mountakm tight toned and de trees MAR wird tom sisibilky in the north. south end mid quadrants of Ms tie palm. 10101108and suquendets in the tk pattern are lased an position repels reaked from pileb in *see mess. Pleb are owl to mile newels psalm repeds tding detente and *Men from the field and to be vighnt for '1214 other filed itetMty M Me arse. The °Mel tem may be mble to preside rime! seperaden to toadin Om arm Large and Mph mamma sett may dip Rory 111 into ist de wed of arpt and dip on 310' Mimi ewer tit We. MOCK ATVI. 13.4ow PPR tor Cluitstfid Trandst colqpiy aelL FIKIaltsniled eardnoway. CLOSED to Mr Order Ops nth more than 30 pastior seek 0100-150029 acept 12 hews PPR cell arpt award 916-541-406M PAN written approval mud be 'Mined hem Amt mow, kr touch and go Ides for Jet and alt met 125001x. Noise indolence in W ad. fle* walks amt. Nein Seek 1600-040072-1114 0100-15004- 77.101(A). NM maws at smou OM 1.7 ME FM FAR 36 apdi dm Weans. Noise Wing MI. Adt 77.1 OS(A or under; ansipmey/mmer gmenwimmt sett mempled from dip swim. Operators of alt with War 'mem lid do not mod S4 011(A) are encourapd to .1130 dsmandrab wind TVL NOISE mordring eipipmmt In oentkm acme r TVL. Adt net appearing le meet S4 NYE 01(A) WAWA law 20 mks. IM125 MUMS 01111Wormine. Fakes. Gulfileem, MOM. Wye (mad Ws). 7.4 DMA MAIM MC 111.5727. DC 9-10. 30. 50. Corwin Fairdild F-27-21. de. Mlle adt mom Ma shirelne d or dove 7500' for noise elstement Adt diewths in Rey 36 remsaded upon maim orange arm apprearably ens an mile pees Opal% end el ow, turn left to 320' and follow wafts 1 e We darallne. Adt Alb and wain ewer ITV1 7641± 1 DNA A Ma nemfts until tesehlts 7500' rho ever the Meehan before der.* come. This Wo WI be perlibil *u the F90. This dues net apply to Soil remaining in the end tic pattern adept the erawilld him wit not be mode prior to 41 medibig end of ray at NCO' er above. Nomad nes Rey 111 bawds left dtradwind dem left croweind turn should 661S A . 10067 not be mode will reeding south arpt Wunder/ and 75001ASL. p aufacimi daub le not wished altar pd for crosswind ban tea di Li Mend alb appetindialy 1.5 miles south le a Eplf wase Mae you may &de to 11174 open allthde and sate tree et Intentlene, repent Inds sok course/1M direction. ACTIVATE M1RL Ray 111-36, A 1 7377 ± Wad and VAR key 11 when ha ded-113.4. NortMouth Wady unlei. TPA-7500(1236) knell aircraft pen 11000(1736)framsit/hIgh milkmen@ aircraft. Parking foe. Control Zone effective 16000400ZZ Mil 111111111111111111110 'M11 (916)541-3302. 101181 caromesecre 111.4 SAOIN122.95 MRS (11NO) Tel free dl, del 1-100-521-1599. NOTAM FILE NI MEV6264 j riwsah Idte hap WI 122.1R 1I32T 011910 FSS) MUSD AP110A04 KINGS ONSAINICIINWMP/WP0111 127.95 (West), 1211.11 (East) Mains riahl tan te 13E40 vie Mt 30.4 DMA 1/111116111111 116.4(160004000$) 11190* 121.9 headlno Oar and 1.1V1. north MOO I PI MMIA11616 IMMO! NOTAM FILE NI ...... 14V1 1.7 DAIS swim. mod WA 13.4 DME MQ9 6362 deli hi helding petoorn. 3)191111TAC 1132 U LTA Chen 79 39'10'50"N 120'16'07"W 125'21.4 NM to W. 111150/161 imt WA 1.7 OW I 6367iI I I Rode forecast only OS0043004. 1.1% 7.4 DME TOZE UMW 1002 Chen 26 OW Roy 111. 4.1.014 i.11,12 ma 1 6234 I 1' '''' I recedes Turn NA I I 4 1 4420Ca4....t """'L-4.4A 61114-13NIA-4..-/3. NM CAROM A I ] C D

LIS 7910.51726 moo,* 2226(2304 1141104 OSCUMOt 790041716 (111004) nia(23oo.$) oeller% 17r 4.4 NM A4/13 34 Avid:14rei itlioml et alit& No NNWMeding ohlhilky redudon ler lead tandliens not authorised. MR Ivry 36 When oadrel sus wit in GINA arse ter .,eaters with apparent weather 643±A Malt'," MN g Zoreto, peaiwe net ethwsed. Ma. Rey 11136. MAW end VAE het 11ACTAF. 10'111E1M ir] an X Nin,s.. NUM MIA TAHOE. CAUPOSMA I.DA/DME-2 RWY 18 38.5411-120."SOUTH LASE MCl/LAKE TAHOE age

FIGURE28.-LDA/DME-2 RWY 18 (TVL) and Excerpt from A/FD. 212 213 =lino smAkarr-wicotmco COUNTY meow porn LOC BC RWY 14 AL-1177 (FAA) SAMMY, Atunme MARYLAND Mist m* cow 11794 $14.0 mussuffacommocontaatu (SLY) 4.3 SE UTC-5(-40T) 1111018111 MC Olt 38.2016114 25.30.3teW 114.55 WATtILOO 144411.1,4111. NUM, MI 0419 52I $4 NIL 100U.. JET A CFRIndec A 1083111111112 2457014 1123 ATI 233 (QM Own 73 14-* 1155005150 (ASPII-CONC-PFC) 3-34. D-54. 01-99 heft SW* AEI. VA31(840-11A 3.06TCH 54'. Tress. MUM MAWR. Tress. IMO* 1150=150 (IMI)3.30.030MM. ROM NEIL VAII(V41.)-11.4 3.0'704391. Tress. INN* REL. VAM(V41.)-6A 3.0.TCH 39'. Tress. AMPORTIVIMMOR Attended 1100-03004. CAUTION: Midi on and in vicinity of 51$. NumerousmW4ry Makin on and in adnity el apt Airport CLOSED le unscheduled ar cards op OM more than 30posenvpr sots swept 1 has PPR cal mot wow 301448-4827. Rey 14 VAS unmonitored. Mqr 123.6 5 timeson ma 3 times off. Nvri 14-32 middle 11*d elm combed outer Mrds PFC. Deer on Orport. Nauman militarysetivitiss on end in vicinity of IRA 00111111116'Moni02w 123.6 OWN 12225 111111101,181 ($11) in sipt. 123.6 LC 742-8710. (1100-03002). NOTAM FILE SOY. 0111111110 IN Mt) Tell free ed don 1-800-WX-IIRIEf. (0300-110MP. 114.5 1419 211. 111111 1108 122.11114.57 (NEWPORT NOVO Chen 12 IMINIIM MO 1223 1223 0113111810 0 F8i) IMMINEMPAMMN 127.95 (120004004) SWIM. 118 55 11181111110111CINI00NN/W GIN 117.7(0400- 12000 11111/1111111111111119 NOTAM FILE NY. VHF/DS Pe LEESBURG MS 11111111TM 111.2 sr Chao 413$ W4" 75.30139°W at ed. 50/03W. VOR portion unusable 290 -320 beyond 10 NM baba 3000'. 01111M1181116 278 SO 38.16'43f1N 75.14'22"W 318* 5.7 NMI 1011.2146? Rey 32 WM COWIE NOS SC meals *fond 13 NM below 3600'.

BACK COURSE

NAME ALTERNATE MINIMUMS vreOlr4i tt...d°73NA% lealow 3300 fire1 .(1C) NINO INT Div 32I sr 10 me mum drveo404 One mini* I almInno MA Awn no 301:63 TN SAY 136' 4.7 NM SAUSBURY-WICOMICO COUNTY REGIONAL, Molding an 1 4435 ONO ikon SOY VOITAC end hom MP NAIL 120AAn' MD YOR Rwy IOC 91C)-ihvy 14 t.'"." .13614...... 1 VAR Rwy 29" ,r *C91994,7 C. 400-214, Category 0. 1100214 "CoMosory D, 400-211 --I

GAMOW: A 344 $40.1 1140-1 VI 540-2,4 m (100.1) 792 iso)M fin4104-0P214 711 2)0 1101 11404 14 $40214 int MUM 74* poo-1) (030-114) 741 $102414) 714 (000214) 061 SINNA 400-1 352 (4001) r2400114 mo) RIR Ivey. 5, 14 owl 93 AIOt ilwra 543 sod 14-32 01111/40 020 001 Mr so AAP 4.7 PO $1111213.1) 4100.1) 1 41 polo% 549 04) PPP( 4s31011 241 1.03 1834 0.0C BC RWY 14 34'3094: 75.31'W maul*, 104119 LAND 215 sAuisterr-wicomico COUNTY REGIONAL (airs

Foam 27.-LOC BC MY 14 (SBY) and Excerpt fromA/FD. WICHITA 53/404041114ENT OCT) XhsRWY 191. AL-0117 (PM) WON& KANSAS MONA MP CON WICHITA 90009Pre.11T (.lT)saw uTC-60101) 37.39110°N9723'5nv INONA 1357 313.1to-wir VIM SAS OW-1W 1332 II So HILL 10011, JET A MOOAS OX 1.2.3.4IRA CFR IndecC 114441,bN WICNIA WWII 1191114416 110.3001(150 (COO C-CINVD)5-100.0150. DT-250 155L CL Nu SPA I. I ALM. TOL Anttrav MIT MR MOAN. Nat*. ONDOON 11 NM 11111511141: H7302X150 (C014-011YD) 5-100. D-176. OT-300 HIRL 011, Mom vat 5004 191111 REIL. VASI(V41.)-11A 3.0TCH 55'. Antenna. 1 1436 Itti,1X1W VANC) S-100. D-150, OT-250 OWL -- MS UT ft REL. 15511(64L)-11A 3.0T01 3913a v5316610-GA3.0TCH mu MW ST NNW! Ationdsd continua*. Adt carrying Inmirdoua or splashy cargo prohibited. night Notification Shako (AOCUS) ovollablo. INANE INA 151111105 U.WAS. CUMINCANIS Ali 125.15 241011 122.95 A IN MAN, (ICT) on opt 122.65. 122.2. 122.15 LC 9424131. NOTAM FILE T. 113.0 1CT Gan 03 A2549 NAM MP MOON 120.6 (010°- loran' and below W IAS 010' -US') 126.7 (190' -009' )134.6 (E 1111 our -Or ItECH1 ite 4500' Nei Wow) 134.45 (010e-1119' above 4500') A2537 !NMI MAU 111.2 NOUN 121.9 oat 41,103 7.1 WE WC In 125.7 3300 MP WON 120.6 (010' - 169.4500' and below) 124.7 (190 - 009')134.45 (010 -1119 above 4500') 124.75 001 MM dc W COL NM Ale44 aI IWO MISTS NIMIATION NOTAM FILE ICT. UMW 1131 CT Chan $5 37'44'43"N 97'35'01''W121'9.1 NM to fit 1470/7E FEU 11111011/1141) 332 IC 37.34'42NN 97.27'20NYI012'4.1 NM to 1Id UN= 110.3 I-ICT Chan 40 Nary 015 LOW PICK 11011. Tarn:. 1621 Chen40 U 109.11461111wi OIL LI 110.5 NOV Rwp 195. NIS Chan 2SY Rory 191...... ccervwxr IMAM Emory froduency 124.5 nat MI at PIS. 1NAI . ,...... 1

3300 to Korchi lot ; °Iv') _ lOM POO 9 '... LIo. lig F.5DAN

Rev 1332 mossPPIOACH Ilemoin %NAN 10 NM NM (hop 14 end 101. Cieb to 33005Now Mot NW eN lops ION*Ad hold. (02/11 Ivry IL eel It Also , 392(1 t#402 2 DM! 193 to . ,..

I rot "IIf 3 ifa =11 00 $ IONA 4 h 041100112 A 1 Cif aleAlt...":11. *MS IN 1359-3/4 no (3001) las 1/40414 542m 1600-1361 (4041) 361(400119) ..'"/'Art 1740.1 I 3/41001 1 1500.110 1903-2 =cum 400 (200.1)I446 (J0M)( NI (50011) NO (11:04) ii 1

PAP to NAP 3.1 NM OWN Era El CF71 CIA hernia 5106 3124 243 T- 3751144711/W W1011243AN5*1 IMIS RWY 19l Wit1(TA MID-COWININT OCT4

FIGURE 28. -PALS AWY 19L (101) and Excerpt from A/A). 216 217 ORAISTON AMIPIR021 CMOUNA NDB RWY 15 OVKISTOK SOWN OWMPON AN CON 11157 CNNILISTON warmKIM avaLlii01A111/110t $7 NN UTC-1(401) 31113'1eNloorvihs 011118111 MN MA Si0$0 MI 1C0. J0 Al + 011 UM(Seawall C IM/. MAK 530 CON KR UM NKOMO MP111301108-121 0471. '1410. 007-771NM. O. 121.0 NSA CM OK 1017aMr1.02.WINV10-0 33' 7C11111. TIM Mufti &Am 11111 1177a waree-et3.0 7C1111'. boa Mullm KIN AIR WOO 10011111010,110310)8-12S. 0471. OT-310. 00-7711335. AM 134,75 IAOR 181111.10113110-101 SS'. Um 01113 VAIM10-1014111. Tem A100 -- Mold ememo1. lay 1543 =KO 8.1 TM M ughmum 123 0- 210 Ile AO* We 100 alp 11.. Ow/ MIK, NW puss sloe me Ks 19 War 1010-up. %Om 2 ossKin post. mem arA soy. KW K01060 Knee (AMON arallAh. 11111111111111111111 011111111111010110 111.71 1111NO 11101 *MOO MIS 133 1.13. 132.1. 122.11 3034042M NOMA Fal CHI IAF 013 13 OW moo. *SKY or um11117 (18)43011311l(sear)111.3Owns120.7 (151'4W) 1311.8 (331' .180') Os 0011- 101111 110011 121.1 ON 118.0 NM 411_M IIINIMISKIIIIINOM NOUNruCM. NO/OF 001130.1 FOS MOM 113.1 CM GI. 1!32131811sronew 40/0081 VOR 011410311 SO NM IN MOO' 101416 WO SWIM SOW. 112'4.5 NM lo 37 KM 111DI32111'3011 6301#52.0 IS 1017 KM *ay 15. WM NOW MS MOO SS 1013 KO *ay 33 330 (34) 311

A IN A CHAKISTON 330 113.1 OK Mr

UIv 46 bruit 1CIA1 NANO ANIOACH *NA 101131 aisb* SOO shot shabInsMR \AL07 * 3300.1. 0e 114331. 4.3 NM Wends Wad 13 OMR end el from MI *IA 1324LIA OIS 1600 2.3 113

A COMM O 173 S.' s 410/40 4341100.59 40 /60 'N 400.110 I 540.1 11 6004 WINO 340.1 is4wan 404 pow 334 0110.21 0

11:77.. r5a DAWN 4330 SAO 2.11 1148 140 219 VOITAW15 3211141007W COMM" SOWN CHAIIRSTON APII/INTL (CHB

FIGURE 29.-NDB RWY 16 (CHS) and Excerpt from A/FD. 11111SYME/ROCIONGHAM COUNTY NC MON (NC14) NORTH CAROUNA SDF RWY 31 AL -4329 (FAA) amoM1111. NORTH GROWN "...... Kann 1 I MCKINNON CO NCONION (NC14) 7.8 NW UTC-5(-401) 36'26'09'N 79'50158"W CINCINNATI 6768 64 NG lOOLL, JET Al OX 3 mewls Sr 1343 H52008100 (AVM 112.5 MK rt MR Lk VAS1(1121.)-04 3.75'01 31.1'. Tied depled 200'. Trot MG OR REIL VASI(V2L)(1/13.75*TCH 34'. Usm. IMPORT NM& Mended Mon -Sit 1230744usk. Sun 1800744usk. Emerpmey rapers (919)5854423. For MIX Ray 13-31. VAST New 13.31 and REIL RWI 31 My 122.8 3 tknes 01111111111011M*011011111COM 122.8 NUS RI (110U) Tahoe cal diN 1400462-7272. NOWA FILE RCN. 4111111111161101 12316,122.2,122.18116.21 (RALEIGH FSS) 6 emmoWNW* 120.9 1411114118111WAVAING NOTNA FILE ROU. aumussenveue 1162asoOwn 109 36'02144N79'58e3e'sw018'242 WMtow I 880/03W. NOTAM ME 030. GANN Mme) 423 SW 36'22156"N 79'45'49"W315'5 NM to IN 1013 °GA Rwy 31 1

1 // /

...... "..... Emu 676 awry 13Wes' MISSED MIPROACI4 of 1111111111110 awai tight turnIn2500 'mu,...... wain 10 NM dined SD MA and MM. /Sio M NOS

RUMINT 14.'i -..312"16: 2600 12100 .,or-...... 1 CAROM A I s C D 1120-1) L31 11201432(3w) 1120111 452 (KO 1 iii 452 13001 Vt) 1340-2 CIMINO 13001024 (700.1) 132043/4 1144(700440 66417004) Obledu kW sifffieler Wang en CTNF; Mien nee rreelleble, um Oreeneirete elesaMer *Niko. end imam NI MD& SO Not iriCTNATI Milk VAS Ohl 13-31, Illl Ivry 31.00. NIL Ivry 3 0 ADP Required. MI*In11 3.31. IP ?Al? MAW 41 NM A NA 1040140110112011501100 Mimierl 4441 3:1411 227 I 1:51111:311 3624147,51'W MOM& NORTH CA1101444 SDF RWY 31 REIDSYILII/ROCKINGHAM COUNTY NC MINION(NCI FIGURE30.SDF RWY 31 (NC14) and Excerpt from A/FD. 221 220 SIN -11i) - 1812 -11111 646 1126 %) 54-2 ELEV CO1411$ (700-19i) (900 (900-2%) (900-11/4) (900-2%) ELEV COIL (600-113) (600-2) (600-11/4) (600-2) A. ELEV COL-4111 (70:2-114) (700-2) (703-2) 1231.-MIS (400-3/4) (400-1) (500-3/4) Increase ELEV (50C MT/ NAA 660 835 635 835 635 NAT/ NM 529 529 518 g58 2. Category 2,1434 NAT/ NAA 736 706 700 SR penetrate NAT/ MM 410 421 454 465 setting to MALSR. -11i - -2% -2% only airport MI Rey Minimums. ROAMS 2818-114 31111-114 1111A-1118 1528-1% 1518-2 182111-114 111111-2 16, 3111 3111 1111 altimeter of 011/ ROA= 1144-114 1121-2 1546-2 sou 1110A-1113 1411/40 1421/50 1481/40 1411/40 rvIuNnr0!--, A applies Arndt. threshold Imperative CAT south C B D B 0 CAT B D B D Fold table CRY C C C from 20.1966 EAT C D C C fcr - sector MALSR Approach 1) authorized. 1.1966 SA 411) feet 30.140V 6000 AP1'R().1 In MOO %) RVR COONS (700-14) (700-114) (900-1) (900-214) (900 (900-21/2) not CONAN (600-14 (600-114) (600-1) (600-114) Inoperative MM. CEIL-11111 (700-1%) (700-1) (700-294) (700-1) (800-294) 1211-111$ (400-94) APPPilArm MAY AirportBrown FIELD (700 and Mutt (400-14) (400-1) (500-1/2) (504-1) (500 (500-1) to NT 17.1983 NAT/ NM 660 660 835 835 835 635 circling I. NAT/ NM 529 529 518 511 het+ NAT! NM 736 736 706 706 700 740 forInoperative 1900 NAT/ NM 410 410 421 454 454 465 465 Instrument 32 County increased i(INif MAR 214 Night Arndt 201.-120.0. 2000 mile S. Fulton Rey of -1% % between A Radar IN'. Amdt MV 1100413 28811-54 2111111-114 34181-1 21111111 3118111-1 1106214 16-34. GA ON/ 110A-41$ MIN% 15211-114 1111211-1 1121-1% Use heights ON/ 111013 1141-1i 1141 1526-1 1126-294 1548-1 15111-214 feet 4111A-9I8 1416/24 1411/50 1421/40 1416/24 140150 14811/24 1411/50 visibility INVRIIMENT AIRPORT-BROWN trees CAT A8 D A C A C Rey CAT A C A C I. MALSF to CAT AB AB 0 AB 0 Increased 20as HANTSRELD CAT AB D ABC AB D AB D 5-271. -Civil 222 NC of effect: AR west amennst numerous much S. and 31.- In ACTIVATE COUNTY Nob* as RA[ 10/TC11/1114 not and 1$/T111/014 3. 1111/TC11/1114 WILLIAM NA 1111/7141/101 S-26R NESIONAI. UM authorized 301.6 zone Net 365.5 8-6R plwie 374/4 FIGURE NWT 34 16 RwY 201. 40 Numerous NWT SR 264. 8 Building NOM INTL ANY 26R 271. MR CIVIL not control A. 9R BL 0 MA% Circling When CAUTION: Categories CAUTION: immesh Categories .r/ ASNEVILLig NAGAI-123i ASR CIRCLING ATuNTA/OCKALS-PEACNTREE NAGAR-111.3 ASR CIRCLING alt ATuNTA/IFULTON RADAR-121.0 ASP CIRCLING MANTA/TIE ATLANTA 3ASAR-127.9 ASR APPOIldIX 3

LOADING CONDITIONS WT-1 WT-2 WT-3 WT-4 WT-5

PASSENGERS FORWARD COMPT 18 23 12 28 28 AFT COMPT 95 112 75 122 103 CARGO FORWARD HOLD 1,500 2,500 3,500 850 1,400 AFT HOLD 2,500 3,500 4,200 1,500 2,200 FUEL TANKS 1 AND 3 (EACH) 10,500 11,000 FULL 10,000 11,500 TANK 2 28,000 27,000 24,250 26,200 25,200 FIGURE 32.-B-727 Loading. .

LOADING CONDMONS WT-6 WT-7 WT-8 WT-9 WT-10

PASSENGERS FORWARD COMPT 10 27 6 29 21 AFT COMPT 132 83 98 133 127 CARGO FORWARD HOLD 5,000 4,500 1,300 975 2,300 AFT HOLD 6,000 5,500 3,300 1,250 2,400 FUEL TANKS 1 AND 3 (EACH) 9,500 9,000 FULL 11,000 10,500 TANK 2 21,700 19,800 12,000 29,300 22,700

FIGURE 33.-B-727 Loading.

LOADING CONDITIONS WT-11 WT-12 WT-13 WT-14 WT-151

PASSENGERS FORWARD COMPT 11 28 22 17 3 AFT COMPT 99 105 76 124 130 CARGO FORWARD HOLD 3,100 4,200 1,600 3,800 1,800 AFT HOLD 5,500 4,400 5,700 4,800 3,800 FUEL TANKS 1 AND 3 (EACH) 8,500 11,500 12,000 11,000 10,500 TANK 2 19,600 27,E 30 29,100 25,400 21,900

FIGURE 34.-B-727 Loading.

33 223 r AIRPLANE DATUM CONSTANTS 1 1 PAC 1L E. of PAC 180.9 inches 'Basic Operating Index 860.5 inches 9447r1.0 OPERATING LINIunota ximum Takeoff Slope + 2% ximum Takeoff/Landing CrosswindComponent Moan Takeoff/Landing Tailwind 32 knots Component 12 knots I )IEIGHT LIMITATIONS ,BasicOperating Weight Mourn Zero Fuel Weight 105,500 pounds! 'cilium Taxi Weight 138,500 Maximum Takeoff Weight (Brake Release) 185,70011:1UTZ. /Maximum Inflight Weight (Flaps30) 184,700 pounds) I (Flaps 40) pounds' !Maxims Landing Weight (Flaps 30) 114455,0009" (Flaps 40) 155,000 pound L 143,000 pour

FIGURE 35.Table of Weights and Limits.

224 Appendix 3

PASSENGER WADING TABLE CARGO WADING TABLE.. Number 110111111d of Weight Masnent 1v Pass. Lbs. -Reir Forward Hold Alt Hold Penn= COMMITS'S/ft Catnnoo-581.0 Weight Mn Arm Lba. 680.0 1100.0 5 850 495 6,000 6,908 10 1,700 989 15 2,550 1,484 5,000 3,400 5,830 20 3,400 1,979 4,000 2,720 4,884 25 4,250 2,473 3,000 2,040 3,498 29 4,930 2.809 2,000 1,360 2,332 1,000 680 1,168 Arr Coarerraiver Cornea-1028.0 900 612 1,049 10 1,700 1,748 800 544 933 20 3,400 3,495 700 476 816 30 5,100 5,243 600 408 700 40 6,800 6,990 500 340 583 50 8,500 8,738 400 272 488 60 10,200 10,486 300 204 350 70 11,900 12,233 200 138 233 80 13,000 13,980 100 88 117 90 15,300 15,728 100 17,000 17,478 NOTE:THESE COMPUTATIONS ARE TO 110 18,700 19,223 RE USED FOR TESTING FUR, 120 20,400 20,971 POSES ONLY 133 22,810 23,243

FUEL WADING TABLE LTANKS 1 6 3 (EACH) TANK 2 (3 CELL) eight Aras Matted Weight Anw Moose* Weight Arm Mowed Lbs. -Mir Lbs. -nor Lbe. 1000 8,500 902.1 8,433 8,500 9173 7,799 22,500 9143 20,578 9,000 990.0 8,937 9,000 917.2 8,255 23,000 914.5 21,004 9,500 993.9 9,442 9,500 917.0 8,711 23,500 914.4 21,488 10,000 994.7 9,947 10,000 918.8 9,108 24,000 914.3 21,943 10,300 9954 10,451 10,500 918.8 9,024 24,500 914.3 22,400 11,000 998.1 10,967 11,000 918.5 10,082 25,000 914.2 22,855 11,500 990.8 11,463 11,500 918.3 10,537 25,500 914.2 23,312 12,000 097.5 11,970 12,000 918.1 10,993 28,030 914.1 23,767 PULL CAPACITY (Sao note at Iowa left) 26,500 914.1 24,244 Note, 18,500 915.1 18,929 27,000 914.0 24,878 for Tank 2 19,000 915.0 17,385 27,500 913.9 25,132 wet t°741staft:7215°°lbs. to 19,500 914.9 17,841 28,000 913.9 25,589 18,000 lbs. have been lair- 28,500 913.8 28.043 party omitted. 90,000 914.9 18,298 10,500 014.8 18,753 29,000 913.7 28,497 21,000 914.7 19,209 29,500 913.7 26,964 21,500 914.8 19,084 30.000 913.8 27,408 22,000 914.8 20,121 I FULL CAPACITY

FIGURE 36.-Loading Tables.

35 225 LOADING CONDITIONS WS-1 WS-2 WS-3 WS-4 WS-5

LOADED WEIGHT 90,000 85,000 84,500 81,700 88,300 LOADED CO (% MAC) 22.5% 28.4% 19.8% 30.3% 25.5% WEIGHT CHANGE (POUNDS) 2,500 two 3,000 2,100 3,300 FWD COMPT CENTROID - STA 352.1 AND -227.9 INDEX ARM AFT COMPT CENTROID - STA 724.9 AND +144.9 INDEX ARM MAC - 141.5 INCHES, LEMAC- STA 549.13, AND -30.87 INDEX ARM

FIGURE 37.DC9 Weight Shift.

LOADING CONDITIONS BE-1 BE2 BE-3 BE-4 BE-5

CREW 360 340 350 340 380 PASSENGERS ROW 1 350 300 120 - - ROW 2 260 250 340 370 - ROW 3 200 190 350 400 170 ROW 4 340 170 300 290 200 ROW 5 120 190 170 200 290 ROW 6 400 340 - 170 400 ROW 7 120 190 - 210 370 ROW 8 250 - - 190 340 ROW C - - - 420 430 BAGGAGE NOSE 60 - 80 - loo FWD CABIN 250 100 120 - 200 AFT (FWD SEC) 500 200 250 800 - AFT (AFT SEC) - 600 500 - - FUEL GAL 370 390 400 290 340 TYPE JET B JE) A JET B JET A JET B TEMP +W C +156C -156C +106C +256 C 4......

FIGURE 38.Beech 1900 Loading Passenger Configuration.

226 38 Appendix 3

LOADING CONDITIONS BE-6 BE-7 BE-8 BE-9 BE-10

CREW 360 340 350 370 420 CARGO SECTION A 500 - 800 800 350 B 500 400 200 800 450 C 550 450 400 600 450 D 550 600 400 600 550 E 600 600 200 550 550 F 600 600 200 350 600 G 450 500 200 250 800 H - - 200 250 - J 350 - 300 150 - K - - 260 200 - L - - 100 100 - FUEL GAL 340 370 390 290 400 TYPE JET B JET B JET A JET A JET B TEMP +25'C +5' C +15' C +10' C -15'C BASIC OPERATING WEIGHT - 9,005 POUNDS, 25,934 MOM/100

FIGURE 39.Beech 1900 Loading Cargo Configuration.

. , -.' 227 37 LOADING DATA APT SAOSPAWCANSO INN 5141M1 COUPT. STANDARD SEATING COPT. (APTnano* F.S. F.S. AFT BACIOMOCARCIO 1825 175.4 MD CANT COPT. fay saanasaN: FS. SWAGS COW. 4525 5113 I I 1 ED ED DI CI Ell[]] Ell Ell I' .I MOGAN i I I I I I I I I WES t 1 DO El ED. CD ED CD ED ED

S. FS F.S. F.S. iF 4'7 PRESS 1501177.35 I 1 Riv I i Flo I I 4F5:0 608.5 430 I PRESS. MD. ROW 2 3 4 6 7 9 WO FMS. I 1 1 1 i1 IMO Fa F.S. F.S F.S. F S F.S F S. FS. FE F.S. All PARTMON F.'s in 200 230 203 250 320 350 380 410 440 557.5

SASSAAWCA110.. LOCATION CAPACITY POUNDS CSMIROID (PUMAS. STATION) NOSE MOON* COMM/MEW 150 US FONNA110 CABIN SAGGAGE COMPARTMENT 250 IPS (INCLUDES UP 10 100 POUNDS MUCH MAY SE SUSPENDED FROM CLOTHES ROD) AFT INOSAGECA11130 COMPARTMENT MO SECTION MO 4113.5 - AFT SECTION 830 533.0

NOTE:

1. For compliment loadings which rosuN in only partial utilization of total compartment volume, load Sams must be distributed or fecund in a ~flat to preclude shifting under normally anticipated operating conditions.

BASIC EMPTY WEIGHT 9,225 LB. BASIC MOMENT/100 25823

FIGURE 40.Airplane - Loading Data.

228 38 LOADING DATA CARGO CONFIGURATION

YAxNNIM STRUCTURAL CENTIME/ WEIGHT AND BALANCE DIAGRAM SECTION CAPACITY MN

A 000 F.E 225 B 600 F.S. 256 C 600 F.S. D 600 F.S. 315 E 600 F.S. 945 F 600 F.S. 375 G 900 F.S.403 p. H 900 F.S. 436 J 900 F.S. 456 K 250 F.S. 490.5 L 595 F.S. 533

MAX ZERO FUEL WEIGHT F.S. 210 NOTES: F.S. 240 1. ALL CARGO IN SECTIONS A THROUGH J MUST BE SUP- PORTED ON THE SEAT TRACKS F.S. 270 AND SECURED TO THE SEAT TRACKS AND SIDE SEAT RAILS BY AN FM APPROVED SYSTEM. F.S. 300 2. CONCENTRATED CARGO LOADS IN SECTIONS A THROUGH F.S. 330 L MUST NOT EXCEED 100 LBS. PER SQUARE FOOT.

F.S. 360 3. CARGO IN SECTIONS K AND L MUST BE RETAINED BY BAG- GAGE WEBS AND PARTMONS F S. 390 PROVIDED AS PART OF STAND- ARD AIRPLANE. F.S. 420 4. ANY EXCEPTIONSTO THE ABOVE PROCEDURES WILL RE- QUIRE APPROVAL BY A LOCAL F.S. 450 FM OFFICE.

272 276 200 284 288 292 296 300 304 F.S. 450 CENTER OF GRAVITY - INCHES AFT OF DATUM F.S. 513.5

MAX TAKEOFF WEIGHT - 16,000 lb MAX LANDING WEIGHT - 16,000 lb MAX ZERO FUEL WEIGHT - 16,000 lb 100401140

FIGURE 41.CG Envelope and Cargo Loading Data. 229 23-0 3

=111111111111MI

USEFUL LOAD WEIGHTS AND MOMENTS

BAGGAGE

AFT AFT FORWARD BAGGAGE/ BAGGAGE/ CABIN CARGO CARGO NOSE BAGGAGE COMPART- COMPART- WEIGHT BAGGAGECOMPART- MENT MENT COMPART- MENT (FORWARD (AFT MENT F.S. SECTION) SECTION) F.S. 855 183.8 F.S. 483.5 F.S. 533.0

MOMENT/100

10 7 16 48 53 20 13 33 97 107 30 20 49 145 160 40 26 65 193 213 50 33 82 242 266 60 39 98 290 320 70 46 115 338 373 80 52 131 387 426 90 59 147 435 480 100 66 164 484 533 150 98 245 725 800 200 327 967 1066 250 409 1209 1332 300 1450 1599 350 1692 1866 400 1934 2132 450 2176 2398 500 2418 2665 550 2659 2932 600 2901 3198 630 3046 3358 650 3143 700 3384 750 3626 800 3868 850 4110 880 4255

FIGURE 42. Airplane- Weights and Moments - Baggage.

231 40

A Appendix 3

USEFUL LOAD WEIGHTS AND MOMENTS

OCCUPANTS

CREW CABIN SEATS

F.S. F.S.F.S.F.S.F.S.F.S.F.S.F.S.F.S. F.S. WEIGHT 129 200230200290320350350410 440 MOMENT/100

80 103 160184208232258280304 328 352 90 116 180207234261 288315342 369 396 100 12 200230260.290320350380 410 440

110 142 220253286319352385418 451 484 120 155 240278312348384420456 492 528 130 168 260299338377Cu455494 533 572 140 181 280322364406448490532 574 616 150 194 300345390435480525570 615 660

160 206 320368416464512560808 656 704 170 219 340391 442493544595646 697 748 180 232 360414488522576630684 738 792 190 .,5 380437494551 608865722 779 836 200 258 400460520580640700760 820 880

210 271 420483546609672735798 861 924 220 284 440506572638704770836 902 968 230 297 460529598667736805874 9431012 240 310 480552624696768840912 9841056 250 323 50057565072580087595010251100

Note: Weights reflected in above table represent weight per seat.

FIGURE 43.Airplane - Weights and Moments - Occupants.

41 '232 I

kmilIPHIRMINI11111111111111111111111111111111111111111111111 11111MIDLSEggagg:glagOOSSIOSISISOSIS41191114...."Iiirsratur: mionirmlITIVII::::::iiiigiiiiiilisII .iiii:PI:mem PI:so II II aasa..._ Jor-411,.,.7 4.1. 10111 110 w me:OW! II!me :pommespeopmemem losigromels",t1,1..,A4.1 leOgIS MOSSOOSSE Sags sesgssewOugssawie : iimmulimull; ; a ili;:s::!!!!!!!!* Jui.tatimmumesursi--- aris...... p.aiii...... , ..... !!!!!!!!!iiithatill I !! maawmulammiggOOSSOOSSOOOSSOgesSegggaggp a 1: ri :-._SIBMII:11:1110111:S.: imme .._-=-...gamominiammem SOMISOOgglimg :::::::::::::::::::: aggOSSSOOSI moSaagf OffaSSO ppologiaggrammemengsfiassegmassiiimpose a ::::: MOSSO OOOOO SIS:OOmSaa91:11 immgagraSOWN, MOO massesswesismomesmosissasso .--- emupoossammuseem OOOOOO moms OO LOOnag lOOOOO :grr-i;::!!!!:11:111 gem: 111111:1111::" Sao gOSSMOSSe..-.,WIJIL. AO O SO10 "SOSO OOOOO SOSO OOOOOgliglaggagaggsm .. ,T. sea slogOgg OSSOOSSIlgaglagOSOSOSaSgsgsaavalaonagamsliagam. : OOOOOOO ESSO Mega aggaISSOSSOugliagS..-1 -17'4 ' q.j!nt141,4111mPas@ Oils MOE SOOmEMBOSISSO --o(,,7roulmilimig imasiram., sionsmsegl :11::::::. i SOOSSfagOloggar.- eageopt MOM mOSSOOSmgmgaagmmasSOO..- PS : .- OgISSOSISSOASOSSOSEOPOOSIMSOSOO aims OOOOOOOOOO mgolOSOS OOOOOaSSOMSOI OSSOOSSOSOSSOMOSOalealla .. :SUM OSSOOSOSImOSSOOgaggam ..1- O .--

I Ilimimmii. Appendix 3 USEFUL LOAD WEIGHTS AND MOMENTS

USABLE FUEL

.5 La/GAL 0.1 La/GAL 5.7 La/GAL GA La/GAL

GALLONSIWEIGHTMOMENTWEIGHTMOMENTWEIGHTMOMENTWEIGHTMOMENT

100 100 100 100

10 65 197 66 200 67 203 68 206 20 130 394 132 401 134 407 136 413 30 195 592 198 601 201 610 204 619 40 280 789 264 802 268 814 272 826 50 325 987 330 1002 335 1018 340 1033 60 390 1185 396 1203 402 1222 408 1240 70 455 1383 462 1404 469 1428 476 1447 80 520 1581 528 1605 536 1630 544 1654 90 585 1779 594 1806 603 1834 812 1881

100 650 1977 660 2007 670 2038 680 2068 110 715 7 5 726 2208 737 2242 748 2275 120 780 ,. _ /2 792 2409 804 2445 816 2482 130 845 2569 858 2608 871 2648 884 2687 140 910 2785 924 2808 938 2850 952 2893 150 975 2962 990 3007 1005 3053 1020 3099 160 1040 3157 1056 3205 1072 3254 1088 3303 170 1105 3351 1122 3403 1139 3454 1156 3506 180 1170 3545 1188 3600 1206 3654 1224 3709 190 1235 3739 1254 3797 1273 3854 1292 3912

200 1300 3932 1320 3992 1340 4053 1360 4113 210 1385 4124 1358 4187 1407 4250 1428 4314 220 1430 4315 1452 4382 1474 4448 1496 4514 230 1495 4507 1518 4576 1541 4648 1584 4715 240 1560 4698 1584 4770 1608 4843 1632 4915 250 1625 4889 1850 4964 1675 5040 1700 5115 280 1690 5080 1718 5158 1742 5236 1768 5315 270 1755 5271 1782 5352 1809 5433 1836 5514 280 1820 5462 1848 5546 1878 5630 1904 5714 290 1885 5651 1914 5738 1943 5825 1972 5912

300 1950 5842 1980 5932 2010 6022 2040 6112 310 2015 6032 2046 6125 2J77 6218 2108 6311 320 2080 8225 2112 6321 2144 8416 2176 6512 330 2145 6417 2178 6516 2211 6615 2244 6713 340 2210 6810 2244 8711 2278 6813 2312 6915 350 2275 6802 2310 6907 2345 7011 2380 7118 380 2340 6995 2378 7103 2412 7210 2448 7318 370 2405 7188 2442 7299 2479 7409 2516 7520 380 2470 7381 2508 7495 2546 7609 2584 7722 390 2535 7575 2574 7891 2613 7808 2852 7924

400 2600 7768 2640 7888 2880 8007 2720 8127 410 2665 7962 2706 8085 2747 8207 2788 8330 420 2730 8156 2772 8282 2814 8407 2856 8532 425 2763 8259 2805 8386 2848 8513 2890 8640

SI.

FIGURE 45.Airplane - Weights and Moments - Usable Fuel.

234 43 ...... OPERATING CONDITIONS BE-11 BE-12 BE-13 BE-14 BE-15

BASIC EMPTY WT WEIGHT 9,225 9,100 9,000 8,910 " 150 MOM/100 25,820 24,990 24,710 24,570 2,,240 CREW WEIGHT 340 380 360 400 370 PASS AND BAG WEIGHT 4,200 4,530 4,630 4,690 4,500 MOM/100 15,025 16,480 16,743 13,724 13,561 FUEL (6.8 LB/GAL) RAMP LOAD - GAL 360 320 340 310 410 USED START AND TAXI 20 20 10 20 30 REMAIN AT LDG 100 160 140 100 120

FIGURE 46.Beech 1900 Loading Limitations.

OPERATING CONDITIONS BL-1 BL-2 BL-3 BL-4 BL-5

CREW WEIGHT 340 400 360 380 370 PASSENGER WT ROW 1 700 620 180 ROW 2 830 700 750 800 950 ROW 3 800 680 810 720 ROW 4 400 850 200 BAGGAGE CENTER 500 550 300 200 450 LEFT AND RIGHT 200 250 100 - FUEL GALLONS 300 250 360 400 260 TYPE JET A JET B JET A JET B JET A ,..1

FIGURE 47.Bell 214 ST Loading.

235

44 Appendix 3

LOADING CONDITIONS BL-6 BL-7 BL-8 BL-9 BL-10

BASIC WEIGHT 10,225 9,450 9,000 9,510 9,375 BASIC MOM/100 25562.5 23236.0 22020.5 23499.9 23296.8 CREW WEIGHT 340 380 410 360 400 PASSENGER WEIGHT 3,280 2,880 3,150 2,040 2,4001

PASSENGER MOM/100 6722.5 5418.6 6425.8 4732.2 4580.7 p BAGGAGE (CENTER) 700 600 300 550 650 FUEL LOAD (6.8 LB/GAL) 435 290 220 435 380 TRIP FUEL BURN (GAL) 355 190 190 325 330 LATERAL CG IS ON LONGITUDINAL AXIS

FIGURE 48.Bell 214 ST Weight Shift and Limits.

45 236 196.2 215.4 156.9 REFERENCE DATUM .-50

35.4'

11SEAT

BAGGAGE COMPARTMENT

LONGITUDINAL FLIGHT STATION NOTE: ALL DIMENSIONS LOCATED IN INTERIOR OF HELICOPTER ARE LATERAL LOCATION

Helicopter station diagram

WEIGHT CG MOMENT

WEIGHT EMPTY 9387.5 247.89 2327105

FIGURE 49.Helicopter - Loading Data.

237 46 Appandbt 3

Crew and Passenger Table of Moments

CREW AND PASSENGER TABLE OF MOMENTS (INLB)

CREW SEATS AIRLINE PASSENGER SEATS

FIRST ROW SECOND ROW THIRD ROW FOURTH ROW :FOUR PASSENGER)(FIVE PASSENGER)(FIVE PASSENGER)(FOUR PASSENGER) WEIGHT SEATS SEATS SEATS SEATC LBS F.S. 117 F.S.156.9 F.S. 196.2 F.S. 215.4 F.S. 244.6

100 11700 15690 18620 21 540 24460 110 12870 17259 20482 23694 26906 120 14040 18828 22344 25848 29352 130 15210 20397 24206 28002 31798 140 16380 21966 26068 30156 34244 150 17560 23535 27930 32310 36690 160 18720 25104 29792 34464 39136 170 18890 26673 31664 36818 41682 180 21060 28242 33616 38772 44028 190 22230 29811 36376 40926 46474 200 23400 31380 37240 43060 48920 210 24570 32949 39102 45234 51366 220 26740 34518 40964 47388 53812

Baggage Compartment Loading Table

BAGGAGE COMPARTMENT LOADING TABLE (IN. LB.+ 100)

LEFT AND RIGHT CENTER BAGGAGE BAGGAGE COMPARTMENT BAGGAGE COMPARTMENT WEIGHT STA. 278.0 TO 316.0 STA. 278.0 TO 316.0 LBS F.S. 295.2 F.S. 297.0

50 147.6 148.6 100 295.2 297.0 150 442.8 445.5 200 590.4 594.0 250 738.0 142.5 300 885.6 891.0 350 1033.2 1039.5 400 1180.8 1188.0 450 1328.4 1336.5 500 1476.0 1485.0 530 1564.6 1574.1 550 1633.5 600 1782.0 650 1930.5 700 2079.0 740 2197.8

FIGURE 50.-Helicopter - Weights and Moments- Crew, Passengers, and Baggage.

47 ,238 Usable Fuel Loading Table

USABLE FUEL LOADING TABLE (ENGLISH)

JET A. JET Al.- JP-5 (6.8 LBS/GAL;

U.S. WEIGHT MOMENT U.S. WEIGHT MOMENT GAL LBS C.O. IN. LB. . 100 GAL LBS C.G. IN. LB.: 100

10 68 244.3 166 220 1496 246.9 3694 20 136 244.3 332 230 1664 244.3 3820 30 204 244.4 499 240 1632 241.8 3947 37.1 252 244.4 616 250 1700 239.6 4073 40 272 242.8 660 260 1768 237.6 4200 50 340 237.8 808 270 1636 235.6 4326 so 408 234.5 957 250 1904 233.9 4453 70 476 232.1 1105 290 1972 232.2 4579 80 544 230.9 1256 "291.4 1982 232.0 4597 90 612 229.2 1403 300 2040 233.1 4754 99.7 679 228.2 1546 310 2109 234.0 4934 109.2 743 229.2 1695 320 2176 235.1 5115 110 748 228.5 1709 330 2244 236.0 5296 120 916 231.7 1990 340 2312 236.9 5477 130 584 234.4 2072 350 2380 237.7 5659 140 952 236.7 2253 360 2448 238.5 6839 150 1020 238.6 2434 370 2516 239.3 6021 160 1068 240.4 1615 380 2584 240.0 6202 170 1156 242.0 2795 390 2652 240.7 6383 180 1224 243.3 2979 400 2720 241.3 6584 190 1292 244.5 3169 410 2795 241.9 6745 200 1360 245.6 3340 420 2856 242.5 6927 210 1428 2411.6 3521 430 2924 243.1 7108 218.4 1484 247.3 3673 435.0 2958 243.4 7199

JET IL JP-4 (6.5 LBS /GAL)

U.S. WEIGHT MOMENT IU.S. IWEIGHT OMENT GAL LBS C.O. IN. LB. i 100 GAL LBS C.G.O. IN. LB. ; 100

10 65 244.3 159 220 1430 246.9 3531 20 130 244.3 318 230 1495 244.3 3652 30 195 244.5 477 240 1560 241.8 3772 "37.1 241 244.4 589 250 1625 239.6 3894 40 260 242.8 631 260 1690 237.6 4015 50 325 237.8 773 270 1755 235.6 4135 60 390 234.5 915 280 . 1820 233.9 4257 70 455 232.1 1056 290 1885 232.2 4377 80 520 230.9 1201 "291.41894 232.0 4394 90 586 229.2 1341 300 1950 233.1 4545 99.7 648 228.2 1479 310 2016 234.0 4715 109.2 710 228.2 1620 320 2080 236.1 4990 110 715 228.5 1634 330 2145 236.0 5062 120 780 231.7 1807 340 2210 236.9 5235 130 845 234.4 1981 350 2275 237.7 5408 140 910 236.7 2154 360 2340 238.5 5581 150 975 238.6 2326 370 2405 239.3 5755 160 1040 240.4 2500 380 2470 240.5 5926 170 1106 242.0 2674 390 2535 240.7 6102 180 1170 243.3 2847 400 2600 241.3 6274 190 1235 244.5 3020 410 2665 241.9 6447 200 1300 245.6 3193 420 2730 242.5 6620 210 1365 246.6 3366 430 2795 243.1 6795 *218.4 1420 247.3 3612 435 2827.5 243.4 6882 Extreme limits of fuel C.O. Point of C.O. direction change.

Weights given are nominal weights at 15°C.

FIGURE 51.-Helicopter - Weights and Moments- Usable Fuel.

239 48 Appendix 3

1im/ I I I I MAXIMUMGROSS WEIGHT17.500LBS

16.000

1.000

12.000 /\

MINIMUMWEIGHTFOR FLIGHT -9600 LBS 10.000 . - .--i--,LEFT / RIGHT -3 -2 - 0 1 2 3 LATERAL C. G. STA. - INCHES

FIGURE 52.Helicopter - Lateral CG Envelope.

240 49 Appendix 3

18000

MAXIMUM GROSS WEIGH 17000 17 SOO LBS.

16000

13000

ill 5 14000 i 4.. I- 0I 0 3 13000 $ 0 0

12000

11000

10000 MINIMUM WEIGHT FOR FLIGHT 9100 LBS.

9000 232 234 236 238 240 242 244 246

LONGITUDINAL C. G.STATION - IN.

FIGURE 53.Helicopter - Longitudinal CG Envelope.

241 50 Appendix 3

ALTIMETER SETTING TO STATION PRESSURE

OFE STATION PRESSURE ONH TO PRESSURE ALTITUDE WOONO FT CORRECTION TO 10 ONH ELEVATION ONH IN. HG. pREFfrALTPAIWINARS

Fr As.. 28.81 t° 28.91 199° 976 to979 28.91 to 29.02 IMO 979to 003 29.02 t° 29.12 800 993 to986 29.12 700 906 t0 29.23 to 000 29.23 to20.34 800 990to 004 800 29.34 800 to 29.44 994 to00, 29.44to 400 29.55 997 to1001 29.55 to 1001 29.6r 990 12° 1004 29.66 to 29.76, 990 14304 to1008, 29.76 to 100 29.87 lArne to1012 29.87 to 0 1012to 1015 29.97 tip _400 1015 to 30.08 30.08 to 1019to 30.19 - 280 1022 30.19 -200 t° 30.30 b3 1026 30.30 _40oion to t° 30.41 1030 30.41 t° 30.52 -In 1030 t°1034 30.52to 30.03 -000 1934 to 1037 30.63 1037 to t° 30.74 -790 1041 30.74 to _400 1041 1000 30.85 t° 1045 30.85 -1001045 to 45 t°30.96 1048 30.96to 31.07 -10001048 t°1052 MOMS: ILMATION 2500PT 1050 ORR s 29.48 U1.IC communn = 400 PT. POEM AUT 2900 FT

FIGURE 54.-Altimeter Setting to Pressure Altitude.

51 242 OPERATING CONDITIONS A-1 A-2 A-3 A-4 A-5

FIELD ELEVATION 2,500 600 4,200 5,100 2,100 ALTIMETER SETTING 29.40" 30.50" 1020 mb 29.35" 1035 mb AMBIENT TEMPERATURE +10' F +80' F 0' C +30' F +20' C WEIGHT (X1000) 75 85 90 80 65 FLAP POSITION 20' 20' 20' 20' 20' RUNWAY SLOPE % +1% -1.5% 0 +1.5% -2% WIND COMPONENT 10 HW 10 7W 15 HW 5 PA. 20 HW ICE PROTECTION BOTH NONE BOTH ENGINE NONE CG STATION 590.2 - 580.3 - 594.4 CG INDEX ARM - -3.1 - +5.9 - INDEX ARM REF - STA 580.0, LEMAC - STA 549.13, AND -30.87 INDEX, MAC 141.5 I CG % MAC . STAB TRIM SETTING FIGURE 55.DC-9 Takeoff.

243 52

1,, Appendix 3 1101111ff=111* MODEL DC-9 TAKEOFF SPEEDS 1T1D1 ENGINES

TAKEOFF SPEED - 20 FLAPS EITHER NO ICE PROTECTION OR ENGINE ICE PROTECTION ONLY

TAKEOFF WEIGHT (1000 L$) 60 65 70 75 80 85 90 95 V1 (KNOTS. IASI 104.0110.0115.0120.5125.0129.5133.5136.0 V2(KNOTS, IASI 106.5112.5118.0723,5129.0134.0139.0143.5 V2(KNOTS, mg 117.0121.5126.5130.5135.0139.0143.0147.0

CORRECTION TO SPEEDS V1

-40 -P A -30 20 Ill 1 i MEWl' -20- um

AM _1 0 AmINENT - 20 TEMPERATURE MEM TI INVI AND 0-1 AIRPORT -40 ArlIANI 0 PRESSURE ALTITUDE It AMEN 10- 206°PARPAPM - 10 arfiriArl 30- Varga'

100 as/ill 40 MAWR

AINEPO2 ,1F20 "MOM 2 4 6 $ 4 6 1. ALTITUDE(1000 FT) AM$ ALTITUDE 11000 FT) TEMP

SLOPE UPHILL r 1.5' KNOTS +0.9 KNOTS PER 1% 'DOWNHILL -1.5 KNOTS - 0.9 KNOTS WpElre HEADWIND +0.30* KNOTS 0 KNOTS 0 10 KN TAILWIND -0.S KNOTS ENGINE AND AIRPLANE +0.8 KNOTS +O KNOTS _SE PROTECTION 0 i EXCEEDS V I , SET VI EQUAL TO V a

FIGURE56.- Takeoff Speeds.

53 244 OPERATING CONDITIONS G-1 G-2 G-3 G-4 G-5

FIELD ELEVATION FT 1,050 2,000 4,350 3,050 2,150 ALTIMETER SETTING 29.36" 1016 mb 30.10" 1010 mb 29.54" TEMPERATURE +23' F +10' C +68' F -5' C +5' F AIR COND ENGS 1 AND 3 OFF ON ON ON ON ANTI-ICE ENG 2 ON OFF OFF ON ON GROSS WEIGHT (X1000) 140 190 180 160 120 6TH STAGE BLEED OFF ON ON OFF OFF FLAP POSITION 15' 5' 25' 15' 5' CG STATION 911.2 882.2 914.8 232.9 925.6 LEMAC - STA 860.5, MAC 180.9" ,

FIGURE 57.B-727 Takeoff.

245 54 ApPmullx3

TAKEOFF EM, !PEEN AND STAB TRIM SETTING T K IPR 3 AIROLNOD ON iiiIGEMPRICIFIRSIGIRFIR kr* -4000 IFEEFFIERRIFFFIRIRRIfiFFIFORRIRRiiii , .1.

1000 IRIIIIEWIRHERPFEHROMPRIPHRIRFRIRIFI 3000 11111MIREFFIEFFIFERIWIFIIFFIFFIFIRE NPR NM CORRICT1006 ONO 1 I 3 NNG 2 POBSSURE AIR CONDITIONING OPT..04 ALF-0- IT Cl? MINE ANTI -ICE ON .03 .11, 0 TO 11 (10VE RTIPIND 401111511)4S . ..) 51 MUM MI I FA NITA STA op LMIS MAIO ON MP INSTAALSOS 7 TO 0 ' 116 I 10 7 104 teC TO TO 1 OAT MAWR IT 54 .43 .42 2$ 2S 40 'P6S -10 41 42 43 S TO 7 TO 07 08 III 23 OD TO IVig Vito V2 4 :4S -32 3 TO S .1: 11: Oi 1:1 114 1:0' ANTI -RID OPERATION 4 Wil 0 OD

I TO A 1."*.,401"11111017°L"""iinTO S0 "C.44 211 2$ 41 42 44 "I 114 00 100 120 .4 TO I TO TO STAB TRIM 'C.44 37 JO 41 G1206 112101T CG FLAPS ?LAPS V V V V .V V V oV V V oll V 1000 41... I j i I It i 1 5 IS /20I25 8 2 1 II 2 210 16175 164 175 200 160 171 142 171 110rotAlirtr 0 1/4 400 115 167 157 _147 11 147 12 6 1/2 7 1/4 0 100 1 4O 163 152 163 154 163 14 41/4 7 7 3/4 170 144 150 147 150 4:0 16 6 62/4 7 1/2 S 130 150 15 '60 140 1S4 141 133 14) 133 145 153 1 S 1/4 4 1/2 7 ISO 135 140 134 145 13 140 140 140, 20 S 1/2 6 6 1/2 140 124 145 1)0 145 1)2 144 22 S S 3/4 6 1/4 114 144 130 124 140 125 130 124 138 44 4 1/4 S 1/4 5 314 13 12 120 134 121 133 26 4 1/2 4 3/4 S 1/4 lig 24 4 1/2 4 1/4 to1a INj:1 200 ISI 162 153 162 )0 3 1/4 4 4 1/4 1110 144 13 144 15 14} II: 131 1 1/2 3 314 . 4 180 141 1S4 143 154 148 I )4 3 1/4 ) 1/4 3 1/2 170 121 150 13 ISO 140 150 141 36 2 3/4 3 3 1S 140 160 1)2 146 133 145 IIS 145 1)7 14S JO 2 1/2 2 1/2 2 1/2 40 2 1/2 2 1/2 2 1/2 1:: I:: 1:t 15) Ili Iii 11: 1:: 1:: 42 2 1/2 2 1/2 2 1/2 1)0 117 11) 11 1)2 11 1)1 120 131 111 2:: It: In Hi III 127 "2 "a 200 146 1S7 14 157 100 141 133 143 153 144 153 RAP RETRACTION 140 116 130 11 150 140 140 170 112 20 146 113 146 IIS 145 134 145 160 12$ 142 MAN DS 120 141 1 1 141 133 141 150 12) 1)7 124 1)7

140 lie 133 ' 110 133 , in ti: Ill 0 AI1)0 113 120 114 12 14 127 116 127 300 itg in 1:1 ii: I:: 1" 121 111 122 154501 200 141 133 14) 153 mI IA, 1)7 4o, po pep ill 4 MM 160 132 14S 134 143 124 11174"''''''''' 170 127 2S 141 120 141 131 141 132 140 160 12) 1)7 124 137 124 1)7 121$

1:: It: 2)5 t:: 1:: Ill In 1:1 Ill 111 1) 0 1011 12S 110 124 110 124 112 123 FOR MMUS IMMEDIATELY AP? 120 I I TAMPS" =sum 15' DANK MAINTAIN AT LUST V3 10 AT MEM TWO

FIGURE 58.Takeoff Performance.

55 :246 OPERATING CONDITIONS R-1 R-2 R-3 R-4 R-C

FIELD ELEVATION 100 4,000 950 2,000 50 ALTIMETER SETTING 29.50" 1032 mb 29.40" 1017 mb 30.15" TEMPERATURE (OAT) +50' F -15' C +59' F 0' C +95' F WEIGHT (X1000) 90 110 100 85 95 FLAP POSITION 15' 5' 5' 1' 1' WIND COMPONENT (KTS) 5 HW 5 TW 20 HW 10 1W 7 HW RUNWAY SLOPE % 1% UP 1% DN 1% UP 2% DN 1.5% UP AIR CONDITIONING ON ON OFF ON OFF ENGINE ANTI-ICE OFF ON OFF ON OFF CG STATION 635.7 643.8 665.2 657.2 638.4 ILEMAC STA 625.0, MAC 134.0

FIGURE 59.B-737 Takeoff.

OPERATING CONDITIONS V-1 V-2 V-3 V-4 V-5

BRK REL WEIGHT (X1000) 110 95 85 105 75 CRUISE PRESS ALT 33,000 27,000 35,000 22,000 31,000 AIRPORT ELEVATION 2,000 3,000 2,000 4,000 2,000 ISA TEMPERATURE +10' ISA ISA +10' +10' AVG WIND COMP (KTS) 20 HW 20 TW 30 HW 10 TW 40 HW

FIGURE 60.B-737 En Route Climb.

247

56 Appendix 3

0 TO 60 KTS EPR BLEED CORRECTIONS EPR AIR CONDITIONING OFF +.03 TAKEOFF EPR A/C ON ENGINE ANTI-ICE ZERO

1F -65 OAT -49-40 -31 -22-13 - 4 5 14 23 32 41 50 59 681 77 86 95 104 120 C -54 -45 -40-35-30 -25 -20 -15 -10 - 5 0 5 10 15 20 25 30 35 40 49

2.312.312.312.292.272.242.222.192.172.142.112.072.042.012.012.012.001.951.911.82 1 EPR /111 0EI 1.96 .1111.2.16 ;1221 ALT 5660 AND ABOVE 4000 3000 2000 1000 S.L. -1000 iiFIND TEMP LIMIT EPR FIND PRESS LIMIT EPR USE THE SMALLER OF THE TWO LIMITS

PRESSURE VI, VR, ALTITUDE OAT 2r.. 1000 FT -65 to -19-18 to18 19 to45 46 to 86 APITISICID ON 9 to10 -27 to - 8 7 to 7 8 to34 -65 to -21 to 11to39 40 to 87 88 to 101 7 to 9 -23 1 to 38 F -65 to - - 5 to 7 to to -54 to -2617 to- 2 - to 4 5 to 11 41ta43 -65 to20 21 to 42 43 to 89 to 103 3 to 5 04 to11l 7 to 31 O 39 . a FLAP 11:11.311+111 NEU RIM to 49 RETRACTION/ - to 1 to ., to20 9121131- 4 to 4 to 40,...... 141 to MANEUVERING GROSS WT SPIED FLAPS -1000 LB I V V ireKTS IAS 120 11 11i 1ii 110 11 1A 110 1650.152155 151 153 155 152 154 155 0 210 100' "141-14n47142-143-147142-144-14/143-145-147 144-146147' 1 190 90 131 1 1 132 134.138 133 135 138,133 136 138 134 136 138 135 137 138 2 180 80 122124130122-125-130-123-126-130-124-126130125-127-130125-12030- 5 170 113 117 122 114 118 122,115 119 122 116 119 122 10 160 128 111 15 150 110 144 146 150 145_147 150. 25 140 100 138-140-142 90 _126 128 133 127 129 133_128_130_133.129131)33.130_132_133.. 80 116-118-125117-119125118 121 125119 122 125 120 123 125 121 124 125 FOR MANEUVERS IMMEDIATELY 70 106 109 118 107 110 118 )08 111 117109 112 117 110 113 117)12 114 117 AFTER TAKE-OFF EXCEEDING 15 BANK, MAINTAIN AT LEAST V, + 15 AT TAKE-OFF FLAPS 100130-130-135131-131-135132-132-135.- 15 90 120 121 128 121 122 128123 123 128 124 124 128 125 125 128126 126 128 80- -112-113-119'113 -114-119114 -115 -119r115-116 119117-117-119 TRIM8ITT111 IL. IL: MS. It AMA,1 1' 11211 11 112 113 1 11 1 1 - WanADMAN( NOSEalP 100 124 126 132 126 127 132 CGFLAPS 90 115 117 124 116 118 124117 119 124118 120 124 25 80 I t: . I s. . : I 109 111 116 110 112 116111 113 116 I:11f Iv 11(.11RHIV. 11 11c 1,2 103 10 111 11 6 8 SHADED AREA INDIa TES PERFO' AF C D BY MINIMUM CONTROL SPEED, MINIMUM 8 7-3/4 FIELD 1.7NGTH FOR LIGHTEST WEIGHABOVE SHADED AREA IS REQUIRED. 107-1/2 12 7 V1ADJUSTMENTS 14 6-3/4 1 16 6-1/4 SLOPE 185.3/4 SPEEDS NOT VALID WHEN WIND 205-1/2 WEIGHTS ARE PREDICATED ADD 1KT PER ADD 1 KT PER 22 5 ON USE OP CLEARWAY, 20 KTS HEADWIND 1% UP SLOPE 24 4-1/2 STOPWAY, IMPROVED CLIME OR ARE LIMITED SUBSTRACT 1 KT PER SUBTRACT 1 KT PER 26 4 5 KTS TAILWIND 1X DOWN SLOPE 28 3-1/2 BY BRAKE ENERGY V MUST NOT EXCEED V 30 3 R 1LZILL 1

FIGURE61.Takeoff Performance.

248 57 ENROUTE CLIMB all Mk iongssuesUNITS Wig MIAs. MOOT - La ALTITUDE NIM/141 -PT 21m/110T6 120000 115000 --, 110000 105000 100000 95000 90000 MOO 60000 75000 65000 r 37006 TiNg/rUIL 41/ 5700 al/ 4700 47/ 4100 24/ 3700 21/ 3400 19/ 3100 17/ 2800 16/ 2500 14/ 2300 12/ 1900 e1sT./LA6 261/162 162/364 162/362 140/360 124/376 111/376 100/377 60/376 82/376 67/374 36000 TINE /PULL 141/5900 33/ 4900 40/ 4300 2S/ 3900 22/ 3500 20/ 3200 18/ 2900 16/ 2700 15/ 2500 14/ 2300 11/ 1900 DIST./TAS 246/386 164/383 164/381 443/379 127/328 114/377 103/326 93/375 84/324 22/374 , 63/373 ..--4--- 4. - 35000 l'im7/117713/-1 5100 49/ 4500 45/ 4100 A 43/ 370021/ 3400 16/ 3100 17/ 2600 16/ 2600 14/ 2400 13/ 2200 Dist./TAs 192/382 466/380 147/328 11/ 1600 131/377 117/376 106/326 96/374 07/373 80/323 73/372 60/371 14000-417r7u6 129/ 4700 '46/4300 43/ 3600 41/ 3500 un, 16/ 3200 18/ 3000 16/ 2700 15/ 2500 141 2300 12/ 2100 10/ 1800 DIST./TAS 171/376 160/327 134/376 120/375 106/374 99/373 90/322 02/322 26/321 69/321 62/320 33000 INM /PULL / 4400 24/ 4000 42/ 3700 40/ 3400 18/ 3100 17/ 2900 15/ 2700 14/ 2500 13/ 2300 12/ 2100 10/ 1700 001T./TAs 163/326 137/379 123/374 112/373 102/372 93/371 65/370 76/370 71/369 66/369 94/366 32000 TINE /PULL )26/4200 43/ 3900 41; 3600 19/ 3300 17/ 1000 16/ 2600 13/ 2600 14/ 2400 12/ 2200 11/ 2000 DIST./TAS 139/374 126/372 114/371 104/320 10/ 1700 96/320 87/369 80/368 74/368 67/367 62/367 51/366 31000 TINE /PULL113/ 4000 41/ 3700 49/ 340018/ 3200 16/ 2900 1S/ 2700 '14/2500 13/ 2300 12/ 2100 11/ 2000 9/ 1700 DIST./TAS 126/371 417/370 107/369 98/368 90/367 62/367 76/366 70/366 64/366 59/366 49/164 30000 Time/run 22/ 3900 20/ 360001/ 3300 17/ 3100 16/ 1800 15/ 2600 13/ 2400 12/ 2300 11/ 2100 11/ 1900 0112./TA6 116/368 109/367 100/366 9/ 1600 92/366 64/166 26/364 72/364 66/363 61/363 56/363 47/362 29000 TINE /PULL'1/ 370019/ 3400 48/ 3200 46/ 300015/ 2700 14/ 2500 13/ 2400 12/ 2200 11/ 2000 10/ 1002 DIST./TAS 111/366 102/364 93/363 9/ 1600 86/363 29/362 73/362 68/361 62/361 62/361 63/360 44/360 28000 TINE /PULL 19/ 3600 10/ 3300 17/ 3100 15/ 2900 14, 2700 13/ 2500 12/ 2300 11/ 210011/ 200010/ 1800 [M./LAS 102/362 95/361 88/360 8/ 1600 61/360 76/359 69/369 64,359 59/356 64/368 60/368 42/362 27000 TINL/rugL 16/ 3400 47/ 3200 46/ 3000 15/ 2600 14/ 2600 13/ 2400 12/ 2200 11/ 2100 10/ 1900 9/ 1800 6/ 1500 DIST./TAS 96/168 99/368 62/367 76/357 71/356 66/356 60/366 56/350 52/355 47/355 40/365 26000 ?Ims/PULL17/ 3300 16/ 3000 15/ 2800 14/ 2600 13/ 2500 12/ 2300 11/ 2100 10/ 2000 10/ 1800 9/ 1200 7/ 1400 Cirr./TAS 81/364 82/364 26/363 70/363 65 /352 60/362 56/352 62/362 48/361 44/351 37/361 25000 Tims/rusc 16/ 3100 13/ 2900 04/ 2700 13/ 2600 12/ 2400 11/ 2200 11/ 2000 10/ 1650 9/ 1000 6/ 1600 7/ 1400 DIST./TAS 81/360 /6/350 70/349 66/349 60/349 56/348 52/348 48/348 45/348 41/346 36/3.2 24000 'TINE/PULL15/ 3000 14/ 2800 13/ 2600 12/ 2400 12/ 2300 11/ 2100 10/ 2000 9/ 1800 9/ 1700 5/ 1600 7/ 1300 Dirt./TAs 76/346 69/146 66/346 60/346 66/345 52/346 48/346 46/344 41/344 38/344 32/344 23000 TINL/OUCL 14/ 2000 43/ 2700 43/ 2500 13/ 2300 T 11/ 2200 10/ 2000 9/ 1900 9/ 1800 8/ 1600 11/ 1600 6/ 1300 DIST./TAS 69/342 64/342 60/342 56/142 52/342 40/341 46/341 41/341 16/341 36/341 30/361 22000 Timg/FULL 14/ 2700 13/ 2500 42/ 2400 11/ 2200 10/ 2100 10/ 1900 9/ 1800 8/ 1700 8/ 1600 7/ 1400 6/ 1200 DIST.prAs 63/336 69/339 66/338 61/338 48/338 46/336 41/316 36/338 36/336 33/310 20/337 21000 Timg/ruCL 13/ 2600 12/ 2400 41/ 2300 10/ 2100 10/ 2000 9/ 1900 9/ 1700 8/ 1600 7/ 1500 7/ 1400 6/ 1200 DIST./TAS 611/336 54/336 51/336 47/336 44/336 41/336 38/336 36/336 '134 30/334 26/334 20000TINE /PULL12/ 2600 11/ 2300 41/ 2200 10/ 2000 9/ 1900 9/ 1800 8/ 1700 7/ 1600 ,/ 1400 6/ 1300 6/ 1100 DI6T./TAS 64/332 50/332 42/312 44/332 41/332 30/332 36/332 33/331 30/331 28/331 24/331 19000 Time/PULL 11/ 2400 11/ 2200 10/ 2100 9/ 1900 9/ 1800 0/ 1700 8/ 1600 7/ 1500 7/ 1400 6/ 1300 S/ 1100 DISIWTAs 49/329 46/329 43/329 40/329 37/329 39/329 33/328 30/328 28/328 16/328 22/328 _ 19000 TINL/Pusc 11/ 2200 10/ 2100 9/ 2000 9/ 1900 6/ 1700 6/ 1600 7/ 1500 7/ 1400 6/ 1300 6/ 1200 S/ 1000 DIST./TAS 46/326 42/320 39/326 37/326 34/326 32/326 30/326 28/326 26/326 24/326 20/325 17000 TIms/run 10/ 2100 9/ 2000 9/ 1900 0/ 1800 8/ 1700 7/ 1500 7/ 1400 6/ 1300 6/ 1200 S/ 1200 S/ 1000 G1ST./TA6 41/323 39/323 46/323 34/323 32/323 29/323 27/323 26/323 24/323 22/323 19/322 16000 Time/PULL 9/ 2000 9/ 1900 8/ 1800 8/ 1700 7/ 1600 7/ 1500 6/ 1400 6/ 1300 S/ 1200 S/ 1100 4/ 900 DIST./TAS 37/320 36/320 33/320 11/320 29/120 27/320 25/320 23/320 22/120 20/320 17/120 T 16000 Ifing/PUIL 9/ 1900 6/ 1600 8/ 1700 7/ 1600 7/ 1500 6/ 1400 6/ 1300 6/ 1200 S/ 1100 6/ 1000 4/ 900 DisT./TA5 34/318 32/317 30/317 28/317 26/317 24/317 23/317 21/317 20/317 16/317 16/117 -.. 14000 TINC/rueL 8/ 1800 8/ 1700 7/ 1600 7/ 1500 6/ 1400 6/ 1300 6/ 1200 S/ 1100 S/ 1100 4/ 1000 4/ 800 DIsT./TA6 31/315 29/315 27/315 25/315 24/316 22/316 11/316 19/316 . .16/314 17/314 14/314 13000 TINL/rutL 8/ 1700 7/ 1600 7/ 1500 6/ 1400 6/ 1300 6/ 1200 S/ 1200 S/ 1100 5/ 1000 4/ 900 4/ 800 DIST./TA6 27/312 46/312 24/312 23/312 21/312 20/312 19/312 17/312 16/312 16/312 13/312 12000 Timg/rucL 7/ 1600 7/ 1500 6/ 1400 6/ 1300 6/ 1300 5/ 1200 5/ 1100 6/ 1000 4/ 1000 4/ 600 3/ 800 OHM/LAS 24/310 23/310 22/310 20/310 19/309 16/309 17/309 15/309 14/309 11/309 11/309 11000 Time/PULL 7/ 1500 6/ 1404 6/ 1300 5/ 1300 6/ 1200 5/ 1100 S/ 1000 4/ 1000 4/ 900 4/ 600 3/ 700 DIST.prAs 22/307 20/307 19/307 18/302 17/307 16/307 15/302 14/307 13/307 12/307 10/307 10000 TINE /PULL 6/ 1400 6/ 1300 5/ 1200 S/ 1200 S/ 1160 4/ 1000 4/ 1000 4/ 900 4/ 800 3/ 000 3/ 700 14119./TAS 19/30S 15/305 17/305 16/309 13/309 14/306 13/306 12/305 11/304 10/304 9/304 6000 TIM/PULL S/ 1200 9/ 1100 S/ 1100 4/ 1000 4/ 900 4/ 900 4/ 800 3/ 800 3/ 700 3/ 700 2/ 600 DIST./TAS 14/300 13/300 12/300 11/300 11/300 10/300 9/300 9/100 66100 66300 6/100 .. 6000 TINL/PUIL 4/ 1000 4/ 1000 4/ 900 4/ 800 3/ 800 3/ 700 3/ 700 3/700 3/ 600 2/ 600 2/ SOO DIST./TA6 9/296 9/296 8/295 6/295 7/296 2/296 6/296 6/296 5 /295 5/296 4/296 .- 16 TimL/ruLL 2/ 600 2/ 600 2/ SOO .4400.4., 2/ SOO 2/ SOO 2/ 400 2/400 2/ 400 1/ 400 1/300 1/ 300 PULL ADJu MUT POO VICO glavATIOM AIMPOOT$ AIRPORT TLLVATION 1 2000 4000 6000 6000 10000 12000 EFFECT ON Tins AmD DISTANCE IS MOOLIOIOLL PULL ADJUITNONT 1 -100 -200 -400 -SOO -600 -700

FIGURE62. Er. Route Climb 280/.70 ISA.

24958 Appendix 3

EMBOUTE CLIMB 18/.11ISA+109 C

8 =ITS 685111 MUSS MONT - 1$ 1511186 1118/24 73000 45000 -80? 00/1010111 120000 113000 110000 105000 100000 115000 110000 85000 80000

37600 TINE TZ!L 42/ 5700 34/ 4700 20/ 410020/ 370023/ 3300 20/ 3000 18/ 2700 16/ 2500 13/ 2100 86/384 78/382 011111.;'he 263/305 206/301 174/380 151/388 133/386 110/385 107/384 13/ 2000 360110 01110 /rugt. 43/ MO30/ MOO40/ 4400 26/ 3000 23/ 3500 21/ 3200 10/ 2000 17/ 2700 16/ 2400 01814158 266/304 211/301 170/380 156/387 138/385 123/384 111/383 100/383 00/382 74/381 .5 30600 0110/1PUBL40/ 0200 34/ 0300 31/ 4600 47/ 4100 24/ 370022/ 3400 20/ 3100 10/ 2800 16/ 2400 15/ 2400 12/ 1000 018141511 273/304 410/300 186/388 162/386 143/305 128/384 115/383 104/302 04/301 85/380 70/370

34006 1106 /r1161 30/ 0600 32/ 4000 20/ 440025/ 3000 21/ 360021/ 3300 10/ 3000 17/ 2700 16/ 2500 14/ 230012/ 1000 67/378 0160.1558 228/300 103/387 168/366 140/304 133/383 120/382 108/381 08/380 80/170 81/370

33660 01118/11015 34/ 3100 30/ 460026/ 410024/ 3000 22/ 3400 20/ 3100 10/ 2000 16/ 2400 15/ 2400 14/ 2200 11/ 1000 01814158 200/387 174/185 154/363 138/382 124/381 113 /300 102/370 03/370 80/378 77/377 64/376

32060 111111/831111. 31/ 4000 20/ 4400 20/ 4000 43/ 3600 21/ 3300 111/ 3000 17/ 2000 16/ 2600 14/ 2400 13/ 2200 11/ 1000 01614158 166/364 160/382 141/361 120/370 116/378 106/378 06/377 88/376 374 73/375 41/374

31010 11111/11015 20/ 4660 t6/ 420023/ 300041/ 3500 20/ 3200 10/ 2000 16/ 2700 15/ 2500 14/ 2300 13/ 2100 11/ 1000 1018141511 160/301 147/370 131/378 120/377 100/176 100/375 01/375 81/374 74/374 70/373 30/372

30000 7188//01027/ 4400 24/ 4000.2/ 370020/ 3400 10/ 3100 17/ 2000 14/ 260014/ 2400 13/ 2200 12/ 2100 1o/ 1700 01814158 132/370 137/376 124/375_,L113/374 103/174 04/373 86/372 70/372 72/371 66/371 53/370

10000 01111/01124 25/ 420003/ 3000 41/ 300010/ 3200 10/ 3000 16/ 2000 15/ 260014/ 2400 13/ 2100 12/ 1000 10/ 1700 018141511 141/375 120/374 114/373 106/372 07/171 00/370 02/370 75/360 60/140 63/360 52/368

21000 0108/01185 24/ 600022/ 3700 20/ 3400 18/ 3100,17/ 2900 16/ 1700 14/ 2500 13/ 2300 12/ 2100 11/ 1000 11/ 1400 01614158 131/371 110/370 100/360 100/360 01/168 84/368 77/367 71/367 65/366 60/366 50/345

27660 111111/11081. 22/ 3600 21/ 3300 10/ 3300 14/ 3000 16/ 2800 10/ 2600 14/ 240013/ 2200 12/ 2000 11/ 1000 0/ 1600 00OT./TA0 121/340 111/367 102/366 63/366 86/365 70/344 73/344 67/364 41/343 56/363 47/343 4 161100 01114,011 21/ 3600 10/ 3400 10/ 3100 16/ 1000 15/ 270014/ 2500 13/ 2300 12/ 2100 11/ 1000 10/ 1000 11/ 1500 01604158 116/363 101/362 03/362 66/361 70/361 73/360 67/360 62/360 57/3511 52/350 44/351

23000 11118/811111 10/ 3404 18/ 320017/ 300015/ 2000 14/ 2600 13/ 2400 12/ 2200 11/ 2000 10/ 1900 10/ 1700 0/ 1300 01614158 101/308 03 /350 85/307 70/307 73/357 67/356 62/306 57/356 53/356 40/355 41/350

24016 Tre/300L18/ 3300 17/ 300016/ 2600 13/ 2601 13/ 240012/ '300 12/ 2100 11/ 1000 10/ 1800 0/ 1700 0/ 1400 _OIST./tA6 02/304 85/354 70/333 72/353 67/353 6 ,352 57/352 53/352 40/352 45/302 36/351

23000 01118/11081, 17/ 3100 16/ 2000 15/ 200014/ 2000 13/ 230012/ 2200 11/ 20410 10/ 1000 11/ 1700 11/ 1600 7/ 1300 018141158 84/300 /11/300 72/330 47/340 62/340 57/3411 53/340 40/348 45/318 41/346 31/346

22000 2488/1081, 18/ 3060 25/ 2600 14/ 260013/ 2400 12/ 2200 11/ 2100 10/ 1000 10/ 1000 11/ 1700 8/ 1500 7/ 1300 53/345 40/345 45/345 42/340 38/345 32/344 0150a". 77/346 11/346 . 46/346 61/346 57/345 21008 0111MS&10/ 2600 14/ 280013/ 2400 12/ 2300 II/ 210010/ 2000 10/ 1800 II/ 1700 0/ 1600 8/ 1500 64 1200 01814158 70/343 60/343 61/342 56/342 52/342 40/342 45/342 42/342 j 30/341 34/341 10/341

20000 0108/0081.14/ 2708 13/ 2000 12/ 2300 11/ 2200 11/ 200010/ 1000 11/ 1800 0/ 1600 8/ 1500 7/ 1400 6/ 1200 8160.M88 64/330 60/330 56/333 52/330 48/130 45/338 41/338 30/338 36/338 33/338 28/338 4 MOO 015g/rugL 13/ 2300 12/ 2400 11/ 220011/ 2100 10/ 1100 0/ 1800 11/ 1700 8/ 1600 7/ 1400 7/ 1300 6/ 1100 01814158 311/336 55/336 51/336 47/335 44/335 41/335 30/335 35/335 33/335 30/335 23/335

30000 1111/1010. 12/ 240011/ 2300 11/ 210060/ 2000 0/ 1800 9/ 1700 0/ 1600 0/ 1500 7/ 1400 6/ 1300 5/ 1100 _4111.4180 51/333 50/333 46/332 43/332 40/332 38/332 35/332 32/332 30/332 20/332 23/332

17000 11101/114MA 11/ 2300 11/ 2100 10/ 2000 11/ 1000 11/ 1700 8/ 1600 8/ 1500 7/ 1400 7/ 1300 6/ 1200 5/ 1000 21/320 6160./066 40 /330 43/310 _ 42/320 30/320 37/320 34/320 32/320 30/320 27/321 20/320

14111 11118/71/11, 11/ 220010/ 2000 0/ 1000 11/ 1800 0/ 1700 8/ 1500 7/ 1400 7/ 1300 6/ 1200 6/ 1204 5/ 1000 _01814TAS 44/327 41/326 11/326 36/316 33/326 31/326 20/326 27/326 23/324 23/326 10/326

13006 moist 10/ 2000 6/ 1000 0/ 1600 8/ 1700 0, 1400 7/ 1000 7/ 1400 6/ 1300 6/ 1200 5/ 1100 5/ 000 018041 40/324 37/324 35/323 33/323 30/313 28/323 26/323 24/323 23/323 21/323 18/323

16008 TINUIVOL 11/ 1000 11/ 1800 8/ 1700 8/ 1600 7/ 1500 7/ 1400 6/ 1300 6/ 1200 5/ 1100 5/ 1000 4/ 000 0111141511 36/321 34/321 31/321 211/321 27/121 26/321 24/320 22/320 20/320 10/320 16/320

13600 0111/0111. 0/ 1800 8/ 1700 8/ 1600 7/ 1500 7/ 1400 6/ 1300 6/ 1200 S/ 1103 5/ 1100 5/ 1000 4/ goo 0181./TA0 /1/318 30/318 28/318 26/318 25/118 23 /311 21/318 20/318 18/318 17/318 14/318 1 12000 0111/1mM 0/ 1700 8/ 1000 7/ 1000 7/ 1400 6/ 1300 6/ 1200 5/ 1100 S/ 1100 5/ 1000 4/ SOO 4/ 000 3481./0A6 20/315 27/315 23/310 23/315 22/315 20/315 10/315 18/315 .6/315 15/315 13/31' IMO TINI/IUSL 7/ 1606 7/ 1500 7/ 1400 6/ 1360 6/ 1200 5/ 1200 5/ 1100 S/ 1000 4/SOO 4/ 000 3/ 700 401814158 20/313 24/313 22/313 21/313 111/113 18/313 17/313 16/313 15/313 13/313 11/313 16060 /188/1881. 7/ 1500 6/ 1400 6/ 1300 6/ 1200 5/ 1200 5/ 1100 5/ 1000 4/SOO 4/ 000 4/ 800 3/ 700 0182./110 21/310 10/310 10/310 18/310 17/110 14/310 10/310 14/310 13/310 12/310 10/310

8000 1101/ItIt4 6/ 1300 5/ 1200 0/ 1100 0/ 1100 4/ 1000 4/000 4/ too 4/ 000 3/ 000 3/ 700 3/ 600 016f./TAO 16/305 15/300 14/360 13/305 12/305 11/305 11/300 10/303 0/300 0/305 71300

6006 0111 /rOgg. 3/ 1100 4/ 1000 4/ 600 4/ 000 4/ 060 3/ 600 3/ 700 3/ 760 3/ 600 3/ 600 2/ 000 01814158 16 301 10/301 11/301 0/301 8/301 8/301 7/301 7/301 6/381 6/301 5/301 s, 130 OTINO/rug& ,3/ 608 _2/ 660, 1/ HO -2 S60 I/ 006 2/SOO 2/ 400 2/ 400 2/ 400 1/ 300 1/ 300 V_ S L'7,401 gLevAllOo AIRPOOTS 11181017 OulvATION 4600 6008 6006 1011011 12600

FIGURE 63.En Route Climb 280/.70 ISA +10' C. OPERATING CONDITIONS T-1 T-2 T-3 T-4 T-5 I

TOTAL AIR TEMP (TAT) +10' C 0' C -15'C -30' C+ 15' C ALTITUDE 10,000 5,000 25,000 35,000 18,000 ENGINE ANTI-ICE ON ON ON ON OFF WING ANTI-ICE OFF 2 ON 2 ON 1 ON OFF AIR CONDITIONING ON OFF ON ON OFF

FIGURE 64.B-737 Climb and Cruise Power.

OPERATING CONDITIONS W-1 W-2 W-3 W-4 W-5

CLIMB SCHEDULE LR HS LR HS HS INITIAL WEIGHT (X1000) 84 86 78 88 92 CRUISE PRESS ALTITUDE 34,000 28,000 32,000 22,000 24,000 ISA TEMPERATURE ISA ISA ISA ISA ISA AVG WIND COMP (KTS) 20 HW 30 HW 10 TW 20 1W 40 HW

FIGURE 65.DC-9 En Route Climb.

251

60 Appendix 3

EN ROUTE

MAX CLIMB&MAX CONTINUOUS EPR A/C AIRBLEED ON TAT °C MAX. MAX. ---- CLIMB CONT. -40 -35 -30 -25 -20-15 -10 - 5 0 5 10 15 20 25 30 35 40 45 50 S.L TO S.L TO 1500 30000 20000 TO 300002.252.232.212.182.152.122.092.041.991.941.901.861.821.791.761.731.701.671.6i 1500 TO 20000 2.302.282.262.242.212.192.162.132.102.072.042.001.951.911.861.811.751.71.66

35000 i 37000 2.242.22 2.202.17 2.142.112.072.021.971.92 IND TEMP LIMIT EPA FIND PRESS LIMIT EPR E THE SMALLER OF THE .44,i"... AND .44 .460020442.°61-Fin ANVE TWO LIMITS

MAX CRUISE EPR A/C AIRBLEED ON

TAT °C -50 -45-40 -35 -30 -25 -20-15 -10 - 5 0 5 10 1E/ 20 251 301 31[40

1.951.91 1.79 P RESS ALT 302.182.162.142.122.102.072.052.021.99 1.85 1.731.68 1.64 1.61 1.5 1.54 [1000 FT 35 i 372.282.262.242.222.202.172.142.112.072.021.971.921.871.841.80, ANTI-ICE BLEED 'AIR COND-BLEED A/C OFF BLEED CORRECTIONS APPLY TO A EPR CORRECTIONS CORRECTIONSAEPR MAX CLIMB, MAX CONTINUOUS, AND MAIM CRUISE EPR SETTINGS ENGINE ANTI-ICE - .08 S. L TO 37000 + .04 2 ENG -.04 WING

ANTI-ICE 1 ENG -.06

FIGURE 66.-Climb and Cruise Power.

402el 61 \ .

TLME, FUEL, AND DISTANCE TO CLIMB JTSD1 ENGINES - NORMAL BLEED DC-9 SERIES 10 - HIGH SPEED CLIMB SCHEDULE CLLMB AT 320 KNOTS IAS TO 23500 FI' ALTITUDE THEN CLIMBAT M .74 ,.. .-. INITIAL WEIGHT = 86000. POUNDS INITIAL WEIGHT = 90000. POUNDS

PRES. FUEL PRES. FUEL ALT. TLME BURNED DIST. ALT. FEET TLME BURNED DIST. mn. LB. N. ML FEET MIN. LB. N. ML 0. 0. 0. 0. 0. 0. 0. 0. 2000. 0.5 133. 2.8 2000. 0.6 140. 3.0 4000. 1.1 287. 5.9 4000. 1.1 282. 6.3 6000. 1.7 403. 9.3 8000 L8 426. 9.8 8000. 2.3 541. 13.0 8000. 2.3 573. 13.8 10000. 3.0 684. 17.2 10000. 3.2 724. 18.2 12000. 3.8 830. 2L3 12000. 4.0 879. 23.1 14000. 4.8 982. 27.0 14000. 4.8 1041. 28.8 16000. 5.3 1141. 32.9 18000. 5.8 1211. 34.9 18000. 8.4 1309. 39.8 18000. 8.9 1390. 42.1 20000. 7.8 1489. 47.4 20000. 8.0 1583. 50.4 22000. 8.8 1884. 58.6 22000 9.4 1793. 00.3 23300. 9.9 1845. 64.7 23500. 10.6 1968. 89.1 23500. 9.9 1843. 64.7 23300. 10.8 1968. 89.1 24000. 10.2 1888. 88.8 24000. 10.9 2013. 71,5 28000. 11.4 2032. 75.9 28000. 12.3 2196. 81.5 28000. 1.2.8 2223. 83.8 28000. 13.8 2389. 92.6 30000. 14.3 2410. 97.1 30000. 15.5 2598. 105.4 32000. 18.2 2613. 110.3 32000. 17.8 2833. 120.6 34000. 18.4 2844. 128.3 34000. 20.3 3110. 139.8 36000. 21.4 3136. 147.8 38000. 24.3 3494. 188.0 ZNITL4L WEIGHT = 88000. POUNDS INITIAL WEIGHT = 92000. POUNDS 0. 0. 0. 0. 0. 0. 0. 0. 2000. 0.3 138. 2.9 2000. 0.8 144. 3.1 4000. 1.1 274. 8.1 4000. 1.2 290. 6.4 8000. 1.7 414. 9.6 6000. 1.8 438. 10.1 8000. 2.4 537. 13.4 8000. 2.5 589. 14.2 10000. 3.1 703. 17.7 10000. 3.3 744. 18.7 12000. 3.9 853. 22.5 12000. 4.1 905. 23.8 14000. 4.7 1012. 27.8 14000. 5 0 1072. 29.3 18000. 5.8 1178. 33.9 16000. 8.0 1247. 36.0 18000. 6.6 1349. 40.8 18000. 7.1 1432. 43.4 20000. 7.8 1535. 48.9 20000. 8.3 1831. 52.0 22000. 9.1 1738. 58.4 22000. 9.7 1850. 62.3 23500. 10.3 1908. 86.9 23500. 11.0 2032. 71.5 23500. 10.3 1906. 88.9 23500. 11.0 2032. 71.3 24000. 10.6 24000. 11 3 73.9 26000. 1949. 89.1 2079. 11.9 2123. 78.6 26000. 12.7 2272. 84.4 28000. 13.3 2308. 89.1 28000. 14.3 2478. 98.2 30000. 14 9 2302. 101.2 30000. 16.2 2693. 109.8 32000. 18.9 2720. 115.3 32000. 18.4 2951. 128.2 34000. 19 3 2973. 132.8 34000. 21.4 3258. 147.4 38000. 22.7 3304. 157.1 36000. 28.1 3713. 181.0 N

FIGURE 67.-High-Speed Climb Schedule.

253

62 Appendix 3

N.,

TLME, FUEL AND DISTANCE TO CLLMB JT8D-1 ENGINES NORMAL BLEED DC-9 SERIES 10 - LONG RANCE CLIMB SCHEDULE CLIMB AT 290 KNOTS IRS TO 26860 FT ALTITUDE THEN CLIMB AT M .72

INITIAL WEIGHT = 78000. POUNDS INTTIAL WEIGHT = 82000. POUNDS

PRES. FUEL PRES. FUEL ALT. 'ME BURNED DIST. ALT. TniE BURNED DIST. FEET MLN. LB. N. NIL FEET MLN. LB. N. ML 0. 0. 0. 0. 0. 0. 0. 0. 2000. 0.5 113. 2s, 2000. 0.5 120. 2.4 4000. 0.9 227. 4.6 4000. 1.0 241. 4.9 8000. 1.3 342. 7.3 6000. 1.5 383. 7.7 8000. 2.0 437. 10.2 8000. 2.1 488. 10.8 10000. 2.8 574. 13.3 10000. 2.7 610. 14.2 12000. 3.2 893. 18.8 12000. 3.4 737. 17.9 14000. 3.9 815. 20.7 14000. 4.1 888. 22.1 18000. 4.6 941. 25.0 16000. 4.9 1002. 26.7 18000. 5.4 1070. 29.9 18000. 5.7 1141. 31.9 20000. 6.3 1205. 35.4 20000. 8.7 1288. 37.9 22000. 72 1347. 41.7 22000. 7.7 1439. 44.6 24000. 8.3 1498. 49.0 24000. 8.9 1602. 52.3 26000. 9.5 1661. 57.6 26000. 10.2 1780. 61.9 26880. 10.1 1738. 81.8 28880. 10.9 1883. 68.5 26860. 10.1 1738. 61.8 28880. 10.9 1883. 68.5 28000. 10.7 1813. 66.2 28000. 11.8 1948. 71.4 30000. 11.9 1953. 74.6 30000. 12.9 2104. 80.8 32000. 13.3 2102. 84.2 32000. 14.4 2274. 91.7 34000. 14.9 2287. 93.4 34000. 16.3 2484. 104.6 36000. 16.9 2456. 109.2 36000. 18.7 2693. 121.3 LNITIAL WEIGHT = 80000. POUNDS INITIAL WEIGHT = 84000. POUNDS 0. 0. 0. 0. 0. 0. 0. 0. 2000. 0.3 117. 2.3 2000. 0.5 124. 2.4 4000. 1.0 234. 4.8 4000. 1.0 248. 5.1 8000. 1.5 352. 7.5 6000. 1.8 374. 8.0 8000. 21 471. 10.5 8000. 2.2 500. 11.1 10000. * -. , 592. 13.7 10000. 2.8 829. 14.8 12000. 3.3 715. 17.4 12000. 3.3 760. 18.5 14000. 4.0 841. 21 4 14000 4.2 894. 22.8 18000. 4.7 971. 25.9 18000. 5.1 1033. 27.6 18000. 5.6 1105. 30.9 18000. 5.9 1177. 33.0 20000. 8.5 1245. 38.8 20000. 8.9 1327. 39.1 22000. 7 3 1392. 43.2 22000. 8 0 1488. 48.2 24000. 8.8 1549. 50.7 24000. 9 2 1858. 54.4 28000. 9.9 1719. 59.7 26000. 10 8 1841. 64.1 28880. 10 5 1798. 64.1 26880. 113 1928. 69.0 28880. 10.5 1798. 64.1 28880. 11 3 1929. 69.0 28000. 11.1 1879. 88.7 28000 12 0 2018 74.1 30000. 12.4 2027 77.7 30000 13.4 2183 84.1 32000. 13 3 2186. 87.8 32000. 15 0 2364 95.7 34000. 15.6 2382. 99.8 34000. 17 1 2570. 109.7 36000. 17.7 2570. 114.9 36000. 19.7 2828. 128.3

FIGURE 68.-Long-Range Climb Schedule. Appendix 3 , OPERATING CONDITIONS X-1 X-2 X-3 X-4 X-5

DISTANCE (NM) 2,000 2,400 1,800 2,800 1,200 WIND COMPONENT (KTS) 50 TW 50 HW20 HW 50 TW 30 HW CRUISE PRESS ALTITUDE 27,000 35,000 20,000 29,000 37,000 ISA TEMPERATURE +10* ISA +20' -10' +10° LANDING WEIGHT (X1000) 70 75 75 65 90

FIGURE 69.Flight Planning at .78 Mach Cruise.

OPERATING CONDITIONS 0-1 0-2 0-3 0-5

WEIGHT (X1000) 110 70 90 80 100 PRESSURE ALTITUDE 30,000 25,000 35,000 20,000 10,000 TOTAL AIR TEMP (TAT) -IF C -23° C -18' C +e C -6* C

FIGURE 70.Turbulent Air RPM. ilia Ira - I se 1114, E k IMAM ELIE 3111Wkik%11vag mown.I loom kMN in .;114 tht 4';"4110,1 I ONNIAiIN 111 NO -.th %VI igItiN pkinve'Ileow Lr r E N I 6VINMIX NULIP 1111 \I WWII . \ MLR A.ilks..1-- Ikirkk-zNanua II 111U1',_ S.: I uwoEL N k OPERATING CONDITIONS 7-1 Z -2 7-3 74 7-5

DISTANCE (NM) 340 850 900 290 400 AVG WIND COMP (KTS) 25 TW 45 KW 35 TW25 HW 60 HW

FIGURE 72.-Flight Planning at .74 Mach Cruise.

TURBULENT AIR PENETRATION

GROSS WEIGHT 1000 L8 S Ni =WNW TARGET SPEEDPRESS ALT 70 80 90100 110 ISAPER lOn VARIATION 1AS/MACM -1000 FT"------TAT FROM TABLE TAT APPROXIMATE POWER SETTING COLDER - -IN RPM C WARMER + 280/.70 35 77.1 79.0 81.0 83.4 -36 1.6 30 77.2 78.2 79.4 81.1 82.4 -23 1.6 25 76.7 77.5 78.3 79.2 80.1 -13 1.5 20 74.7 75.4 76.1 77.0 77.9 - 6 1.4 15 72.7 73.5 74.2 74.8 75.7 1 1.2 10 70.5 71.3 72.1 72.9 73.9 9 1.3 ......

FIGURE 73 -- TurbulentAir Penetration.

257 66 Appendix 3

ABBREVIATED FLIGHT PLANNING .280/.70 CLIMB .74/320/340 DESCENT 250 KTS CRUISE BELOW 10000 FT. 320 KTS CRUISE 10000 THRU 23000 FT. .74 MACH CRUISE 24000 FT. AND ABOVE

MT. N. MI. REC. ALT. TAS KTS AIR TIME huNS. FUEL LBS. 50 6006:7000 279 16 1800 60 6000-7000 279 18 1950 70 10000-11000 373 19 2000 1I III -'6136------90 10000-11000 373 21 2250 100 10000-11000 373 23 2400 i1006-12000 380 24 3550 120 12000-13000 386 25 2750 130 13000-14000 391 27 2900 140 14000-15000 396 28 3050 150 16000-17000 407 30 3200 160 17000-18000 414 31 3350 170 18000-19000 420 32 3500 180 10000-20000 426 33 3650 190 20000-21000 432 35 3100 300 21000 -I9000 439 36 3950 210 21000-22000 439 37 4050 220 22000. 23000 446 39 4200 230 23000-24000 450 40 4300 240 24000-25000 450 41 4400 250 25000-21000 449 43 4500 26000 -17000 447 44 4600 270 20000-27000 447 45 4750 280 27000-20000 445 47 4950

300 28000-29000 443 49 5100 310 28000-20000 443 51 5200 330 MOO-31000 411 5300 330 29000 -31000 441 53 5400 340 31000-33000 55 5550 1'1'1 IN1'1'1 33000-35000 433 62 6250 33000-35000 433 69 6150 33000-35000 433 76 7500 33000-35000 433 82 9100 33000-35000 433 89 9700 33000-35050 433 5100 33000-35000 433 102 9900 33000-35000 433 109 10600 33000-35000 433 115 moo 33000-35000 433 122 11700 33000-35000 433 129 12300 33000-35000 433 135 12165 33000-35000 433 142 13500 TIME AND FUEL CORRECTION FOR WIND .4 TIME TIME X WIND COMPONENT = TM a FUEL FUEL X WIND COMPONENT TM EXAMPLE: DUT. a 280 STILL AIR TIME 43 MIN. STILL AIR FUEL 4100 LBS. A TIME43 X 30 t 449 MIN. WIND COMPONENT20 Ell. ia FUEL 4500 X 10449. 200 LBS. ADD ATIME ANDLSFUEL FOR HEADWIND; SUBTRACTFOR TAILWIND011111111k

FIGURE 74.Abbreviated Flight Planning.

67 258 Appendix 3

OPERATING CONDITIONS L-1 L-2 L-3 L-4 L-5

WEIGHT (START TO ALT) 85,000 70,000_86,00076,000 82,000 DISTANCE (NAM) 110 190 330 50 240 WIND COMPONENT (KTS) 15 HW 40 1W 50 HW 20 TW 45 HW HOLDING TIME AT ALT (MIN) 15 15 15 15 15

FIGURE 75.DC-9 Alternate Planning.

1._OPERATINGCONDITIONS H-1 H-2 H-3 H-4 H-5

ALTITUDE 24,000 17,000 8,000 18,000 22,000 WEIGHT (X1000) 195 185 155 135 175 ENGINES OPERATING 3 3 3 3 3 HOLDING TIME (MIN) 15 30 45 25 35

FIGURE 76.B-727 Holding.

OPERATING CONDITIONS 0-1 0-2 0-3 0-4 0-5

ALTITUDE 31,000 23,000 17,000 8,000 4,000 WEIGHT (X1000) 102 93 104 113 109 ENGINES OPERATING 2 2 2 2 2 HOLDING TIME (MIN) 20 40 35 15 25

FIGURE 77.B-737 Holding.

do- 9 4,. t) 68

S.- Appendix 3

ALTERNATE PLANNING CHART DIST. - NAM 20 30 40 50 00 70 80 90 100 110 120 130 140 OPTM. ALT. 2000 3000 4000 5000 6000 7000 8000 90001000011000120001300014000 TIME: :16 :17 :19 :20 :22 :23 :25 :26 :28 :29 :30 :32 :33 FUEL 2500 2600 2700 2800 2900 3000 3100 3200 3300 3400 3500 3600 3700 TAS 275 280 283 286 289 292 296 300 303 306 309 312 315 DIST. - NAM 150 160 170 180 190 200 210 220 230 240 250 200 270 OPTM. ALT. 15000160001700018000190002000021000220002300024000250002000027000 TIME :35 :38 :38 :39 :40 :42 :43 :45 :48 :48 :49 :50 :52 FUEL 3800 3900 4000 4100 4200 4300 4400 4500 4600 4700 4800 4900 5000 TAS 319 323 326 330 334 338 341 345 349 353 357 361 365 DIST. NAM 280 290 300 310 320 330 340 350 300 370 380 :.00 400 OPTM. ALT. 2700028000280002900029000300003000031000310003100031000310031000 TIME :53 :55 :56 :58 :59 1:00 1:02 1:03 1:04 1:05 1:07 1:02 1:10 FUEL 5150 5250 5350 5450 5600 5700 5800 5900 6050 6150 6250 6351 0500 TAS 388 372 376 380 385 388 392 397 397 397 397 397 397 NOTES: 1. Fuel includes X climb distance enroute credit, fuel to cruise remaining distance at LRC schedule, 15 minutes holding at alternate, and 800 lbs. for descent. 2. Time includes X climb distance credit, time to cruise distance shown at LRC schedule and 8 minutes for descent.1.5 minutes holding is not included in time.

FIGURE 78.-Alternate Planning Chart.

IRS - KTS FF PER ENG - LB/HR I HOLDING I B-727 PRESSURE GROSS WEIGHT - 1000 LB ALTITUDE FT 200 190 180 170 160 i150 140 130 120 1.85 1.81 1.77 1.73 1.691.64 1.60 1.55 1.51 25000 268 261 253 246 238 230 222 213 205 36W3400 3210303028602680 25102340 2180 1.691.66 1.62 1.591.55 1.51 1.481.44 1.40 20000 265 258 251 244 236 228 220 212 204 3630 3450 3280 311029402770 26002440 2270 1.56 1.53 1.50 1.471.44 1.41 1.381.35 1.32 15000 263 256 249 242 235 227 219 211 203 3670 3500 33403170 3000285026802520 2350 1.45 1.43 1.40 1.381.35 1.33 1.301.281.25 10000 262 255 248 241 234 226 218 210 202 3800 36403460 3310314029702810 2640 2480 1.36 1.34 1.32 1.301.281.2611.24 1.22 1.20 5000 260 254 247 240 233 225 218 210 201 38903720 3550 3380 3220306028902730 2560

FIGURE 79.-Holding Performance Chart.

69 260 Appendix 3

EPR IAS KNOTS PP PER ENGINE LB/HR

. , PLIGHT GROSS WEIGHT 1000 LB LEVEL A 115110105,100,95 90 85 80 75 70 65 2.132.072.011.951.901.851.80'1.761.711.671.64 350 234228223 217211210210210210210210 283028101630)46022902180)070j960187017801700 1.861.821.791.751.711.671.641.601.571.541.51 300 231226220215210210210210210210210 27402600 247023702250214.242 ,.. ._ 1 7 ..* 1.691.661.631.601.571.541.511.481.451.431.41 250 229224218213210210210210210210210 237 2 ... 2710261 , . : . . . . , , e I 1.561.531.501.481.4r1.431.401.381.361.341.32 200 227222 217211210210210210210210210 27162590)4903390231012302130.30604200041.920j860 1.451.431.401.381.361.341.321.311.291.271.26 150 226221216210210210210210210210210 27902680257024702380329022203140307020001990 '1.361.341.331.311.291.281.261.251.241.221.21 100 225220215210210 210210210210210210 _28602780167035603470039(432ajaj 1.291.281.271.251.241.231.211.201.191.181.17 050 224219214210 210210210210210210210 i... 4. 1.251.241.231.221.211.201.191.181.171.161.15 015 224219214210210210210210210210210 .3050.29502850.279026702590251024302370.23002240

FIGURE 80.-Holding Performance Chart.

26)0 Appendix 3

NIT/AL FM SWING FULL MIGHT - 1000 LII 1.111GIT Ile 121_gI: 22: :62 2300 32: 421 73, 52: S410 SI: 625 663 7: 66 262S232120 III1615131110 8 S 3 0 62 2323201817 1513 1210 II 7 S 3 0 SS 2120181615 1311 10 8 6 S 3 0 S4 1816151312 10 8 7 S 3 2 0 SO 16IS1312 1C II 7 S 3 2 0 46 15131210 8 7 S 3 2 0 42 131210 8 7 S 3 2 0 36 1210 8 7 S 3 2 0 TRAEI 34 10 II 7 S 3 2 0 FUEL DUMP 30 8 7 S 3 2 0 26 7 S 3 2 0 I 22 S 3 2 0 FUELJ8TTISON 111 3 2 0 11118-14INUTZS 1 I I 4 2 0 4.110 0 FIGURE 81.Fuel Dump Time.

OPERATING CONDITIONS D-1 D-2 D-3 D-4 D-5

WT AT ENG FAIL (X1000) 100 110 90 80 120 ENGINE ANTI-ICE ON OFF ON ON ON WING ANTI-ICE OFF OFF ON ON OFF ISA TEMPERATURE ISA +10° -10' -10' +20' AIR CONDITIONING OFF OFF OFF OFF OFF

FIGURE 82.-8-737 Drift-Down.

OPERATING CONDITIONS S-1 S-2 S-3 S-4 S-5

FLIGHT LEVEL 370 350 410 390 330 LANDING WEIGHT (X1000) 130 150 135 155 125 DESCENT TYPE .80M/ .80M/ .80M/ .85M/ .80M/ 250280/250320/250350/250 320/250

FIGURE 83.Descent Performance. Appendix 3

1 ENGINE INOP

ENGINE A/I CRP

GROSS WEI= 1000 Ill OPTD121 /SA 121 °C AT WINEATLEVEL CET 1:11IFIDO81 -10 I 0 1 10 1 20 PRIME (AMICK) SPEW laAs APR= GROSSLEVEL CIF!' PRESS ALT FT , 80 77 184 27900 26800 25400 22800 90 86 195 25000 23800 21700 20000 100 96 206 22000 20500 20000 18500 110 105 216 20000 19100 17500 15400 120 114 224 , 18200 16600 14700 12200

EtIGIte A/I ON

91211.111121712141iicrrnim i,.-1V AT Nig=ATMEL OFF=MOM -10 0 10mols20 FA/LURE (MOM) SPEED RIM 1.--. --i`e' -I.* U r-. OFF AIR PT

80 77 184 25500 24600 22800 20000 90 86 195 23000 21400 20000 19400 100 96 206 200000 19400 18700 15600 110 105 216 18100 16600 14700 12200 120 114 224 13800 11800 8800 I15500

EICINE AND WING WI ON

=SS WEIGHT 1000 IB OFTB824 ISA Elk O AT DANEAZ MEL CSTIIIIITOCUN -10 I 0 1 10 1 20 FALWRE (AMMO SPEED CAS WOE GROSS LEVEL OFF PRESSALT PT

80 77 184 24400 23400 21400 20000 90 86 195 21600 20100 19800 18000 100 96 206 19600 18000 16400 14200 110 105 216 16800 15100 13300 10700 120 114 224 14000 12200 10300 7200

NOTE:

WHEN ENGINE BLEED FOR AIR CONDITIONING IS OFF BELOW 17,000 FT., INCREASE LEVEL-OFF ALTITUDE BY 800 FT.

FIGURE84.DriftDown Performance Chart.

264 Appendix 3

.80M/250 KIAS .80M/280/250 KIAS a - _ II 'IV: . IV l. n-sqrzarP za.m. PLIGHTp FUEL .4 P.7 III: (etft. FLIGHTTIMEFUELuraros: A.L.J. I I : if Iel I111.1111161111:111a.II I I 07rerirmr.73B.4.1...14:1)1LB q w u. ., Ir. i..,N) 1 1 390 271600 130 134 136 390 241540 121 127 130 370 261570 123 128 129 370 241520 115 121 125 350 251540 116 120 122 350 231500 111 117 120 330 241510 110 113 115 139_,...231480 106 111 115 310 231480 103 107 108 310 221450 100 105 108 290 221450 97 100 101 290 211430 94 99 102 270 211420 90 93 95 270 201400 88 93 95 250 20 '.1390 84 87 88 250 191370 83 87 89 230 191360 78 80 81 230 181350 77 81 83 210 181320 72 74 75 210 171310 72 75 76 190 171280 66 68 68 190 161280 66 69 70 _I 170 161240 60 62 62 170 151240 61 63 64 150 141190 54 56 56 150 141200 55 57 58 100 111050 39 40 40 100 121080 42 42 42 050 8 870 24 24 24 050 8 870 24 24 24 .015 5 700 12 12 12 015 5 700 12 12 12

.80M/320/250 KIAS .85M/350/250 KIAS "STANCE NA. 'Tliit 'P" IFLIGErTIMEFUEL . WIN1 0-)1--1\- d 0'41, FLIGHTTIMEFUEL . \ D 14, d etillIt.. LEVEL LB if tI I's0: 'ftI'l t0: . 5s I I0: 2i/71_ I I : IIIIIIKIlkirtiliPII lUIMI I: 410 22 19 1131- 1i0 123 440 10. Ir 6 390 22 1480 111 117 121 390 211430 103 110 114 370 21 1460 105 112 116 370 201420 99 106 110 350 211440 101 107 All 350 201400 95 101 106 330 201420 96 103 107 330 191390 91 98 102 310 201400 92 98 102 310 191380 88 94 98 290 191390 89 94 98 290 181360 85 90 95 ,270 19 1370 85 90 94 270 181350, 82 87 91 250 181350 80 85 88 250 171330 78 83 87 230 171330 75 79 82 230 171310 74 78 81 210 17 1300 71 74 77 210 161290 70 74 76 190 161270 66 69 71 190 161270, 65 69 71 170 151240 61 64 65 170 151240 61 64 66 150 14 1210 56 59 60 150 141210 57 60 61 100 121110 45 46 46 100 131130 47 48 49 050 8 870 24 24 24 050 8 870 24 24 24 015 5 700 12 12 12 015 5 700 12 12 12

NAPE: FUEL FOR A STRAIGHT-1N APPRCICH IS INCLCDEEL

FIGURE 85.Descent Performance Chart.

73 264 Appendix 3

OPERATING CONDITIONS L-1 L-2 L-3 L-4 L-5

TEMPERATURE +15' C+27' F -8' C -10' C+55' F TAT OAT OAT TAT OAT PRESSURE ALTITUDE 500 3,100 2,500 2,100 1,200 AIR CONDITIONING OFF ON ON ON ON WING ANTI-ICE OFF 2 ON 1 ON 2 ON OFF WEIGHT (X1000) 100 95 90 105 85 FLAP SETTING 30' 25' 15' 40' 30' RUNWAY ASSIGNED 35 04 27 34 09 SURFACE WIND 300/20350/15310/20030/10 130/15

FIGURE 86.B-727 Landing.

EPR BLEED CORRECTIONS 1 ENG2 ENG GO AROUND EPR AIR CONDITIONING OFF +.03 +.03 ENGINE ANTI-ICE ON LANDING A/C BLEED ON ZERO ZERO WING ANTI-ICE ON (FLT) -.06-.04 REPORTED °F -61 -52 -43-35 -25 -17 -10 10 18 27 38 47 55 64 73 83 91 100 119 OAT C -52 -47,-42 -37-32 -27 -23 -18,-13 -8 -3 3 8 13 18 23 28 33 38, 48 TAT °C -50 -45-40-35 -30-25-20 -15 -10-5 0 5 10 15 20 25 30 35 40 50 2.302. y, ,2.30 2.292.262.242.212.19.2.162.13_2.102.07.2.042.001.981.98 1.981.941.901.80

14; 2.3 2.20 2.15 2.09.1121 .0-.40- 411,221 1'93 .. I -1--/-4 .16- 5660 AND ABOVE 4000 3000 2000 1000 S.L. -000 FIND TEMP LIMIT EPR FIND PRESS LIMIT EPR US THE MA LER OF THE TWO LIMITS

LANDING SPEED

REFERENCE SPEED AT GROSS WT FLAP EXTENSION/ FLAP POSITION -1000LB MANEUVERING SPEED 40 30 25 15' NORMAL MANEUVER AND 110 138142 153158 FLAP EXTENSION SPEEDS 105 134 138 149154 100 130 135 144150 FLAP NORMAL SELECT 95 127 131 140145 POS MANEUVER FLAP 90 123127 136 141 85 119 124 132 136 0 210 1 80 115 120 127 132 1 190 5 75 113 116 123 127 5 170 10/15 70 109112 119 123 10 160 15 15 150 25/30/40 25 140 30/40 ADD WIND FACTOR OF: 1/2 HEADWIND 30. .VREF COMPONENT GUST 40 TREF + (MAX: 20 KTS)

FIGURE 87.Landing Performance Chart.

265

74 Appendix 3

1----LANDING DISTANCE COMPARISON DRY RUNWAY

SEA LEVEL 60°F 40° FLAPS ANTI-SKID OPERATIVE. BRAKES & SPOILERS APPLIED 2 SECONDS AFTER TOUCHDOWN. REVERSERS INITIATED 3 SECONDS AFTER TOUCHDOWN. ENGINE SPIN -UP TIME FOR REVERSE THRUST IS 0.3 SECONDS. CERTIFIED LANDING PARAMETERS USED, EXCEPT REVERSE THRUST WHICH IS FLIGHT TEST DATA.

8000

5000

O L. 1 -.MI NOINGW.. 4000 CA ft._ oC > 0 I- BRAKES 3000 _ u I 6' 1 LERs 8,RevE AKE SRO _ +REVERSERS O & 1LERS IBRAKES zO 2000 ,.. zG 5 AIR+ TRANSITIONDISTANCE AIRDISTANCE 1000 "'",IF F

0 100 110 120 130 140 GROSS WEIGHT - 1000 LBS TRAINING INFORMATION ONLY REPRESENTATIVE NORMAL LANDING

FIGURE 8t)Normal Landing - Dry Runway. ippondlx3

NDING DISTANCE PARISON

WET RUNWAY

sEA L 50°F 40°FLUI% ANTI-SKID ooEttAriVES. BRAKES SPOILERS APPLIED SECONDS AFTER TOUCHDOWN. REVERSERS INITIATED 3sED0NO3 AFTER TOUCHDOWN. ENGINE SPIN-UP TIME FOR REVERSE THRUSTIS 0.3 SECONDS. CERTITIEDLANDINGPARAMETERSUSED, EXCEPT REVERSE THRUST WHICHIS RIGHT FLIGHT TEST DATA. **ea

II aY

saw iima 8/40 NON skiais

altee110 120 GROSS WEIGHT1000 1.8s. NOON° 041104144770N ONLY NORMALL LADING

FIQURE Larld100-We° RUMMY.

78 26 7 Appendix 3

LANDING DISTANCE COMPARISON ICY RUNWAY

SEA LEVEL69°F 40° FLAPS ANTI-SKID OPERATIVE BRAKES & SPOILERS APPLIED 2 SECONDS AFTER TOUCHDOWN REVERSERS INITIATED 3 SECONDS AFTER TOUCHDOWN. ENGINE SPINUP TIME FOR REVERSE THRUST IS 6.3 SECONDS. CERTIFIED LANDING PARAMETERS USED, EXCEPT REVERSE THRUST WHICH IS BASED ON FLIGHT TEST DATA.

6000

UJ - J sc.,0 5000 Q. _i 4%66%6 .,&OW S ... GM I" P 06uu 0 1 I- A a. 4 IL. 6S' 2 4000 6 6' < -.40 cc ku --6041 O , ku3000 . zV < H N_ 000 z0 C z AR & TRANSITIONDISTANCE 5 1000 AIR DISTANCE ,

0/ 100 110 120 130 140 GROSS WEIGHT - 1000 0' TRAINING INFORMATION ONLY REFRESEP- I NORMAL LANDING

FIGURE 90.Normal Landing - Icy Runway. Appendix 3

LANDING DISTANCE COMPARISON FLAPS 0 FLAPS 5 FLAPS 15

TOUCHDOWN AT 1000 FEET FROM RUNWAY THRESHOLD SPOILERS AND BRAKES APPLIED 2 SECONDS AFTER TOUCHDOWN REVERSE THRUST APPLIED 3 SECONDS AFTER TOUCHDOWN MAIN AND NOSE BRAKES SEA LEVEL. STANDARD DAY ZERO WIND. DRY RUNWAY ANTISKID OPERATIVE 6000

5000

c MO

FW16 OM* f PA f 4000 + GO f 0. /1 ;Los) WI*" V REFilly ENGINE1141 MO'S F LAPS)4 313"2" . V FIF FIFO 6 4 AS MAO. 3000 ...... Landing Fub,PSA v./EC MS16 LMTDiMhIM

2000

NOTES 1.TOUCHDOWNAT 1000FEETFROMRUNWAYTHRESHOLD 2.SPOILERSANDBRAKES 1 000 APPLIED2 SECAFTERTOUCHDOWN 3.REVERSETHRUSTAPPLIED3 SECAFTERTOUCHDOWN 4.MAINAND NOSEBRAKES 5.SEA LEVELSTANDARDDAY 8.ZEROWIND I 0 I kll 100 110 120 130 140 150

GROSS WEIGHT 1000 POUNDS

TRAINING INFORMATION ONLY REPRESENTATIVE

NORMAL LANDING

FIGURE 91.Normal Landing Distance Comparison.

2 69 78

I ,1 L -0.11111 MEI111011.11111.01111MIIIIIIMMEMBIEW._111111NOMMINIMMIMM MEMOM iE MI mmmEMI rilW,,1111MAIMINFENN FIFA MIIIMMIll 111101011111p11NimprAMMlibiTAI Um" illmmmommilammomm 11111111EMNNIMOMMEVIIINI . 0.MMEIMMEMENOMMIIII IMIIIVAMMIIME EM 111111111.144= IFAMICP01 MUM 111110WI ME . - . - 01111111M IIIUMEMIIIIm 1111111001 MIR ErSh1111 - NUMMI 'Emmy NEE'MEM mu. ME ./ . MM. WWII RIM MOM 71.10 ic MVIIIMIN e- - .:111MEMMM MAME MEM =MAE at . IIMUM0 INNIAMMEI IINWHIli.."100k mumMIAMI MMES.mum SEMMEMEMIN MMMEMMEM Twain MINTmem NM= of _MMEMM- MIMI MMUMimmoEMMMEMMINIMEMMMEMINO MMIIMMEMMMMEMMEMIO MEHM111 SUMIL MOMMOMMEMMIUMM - MMEMMMMEmillimummMMOMMEMEMMI mmummumaimmommilmmMM MMMME EM , MEMMMUIMUMMUMUM INUMENHOMMINENMEMIL MRMIM1- IIMIIIMMMEMM MIMEM MMMEMEMMMIMMMMUM MM MM IIMUMMER INIM . 1 I

. margassumemisom.1 MMMMM v. I, spompsoLpiemolimisimmemolommemommmemmommanam milmosiormallemmLmmosukummemetlimmosmommemsom . :11! IOOMISOOBOMO 11181101111101110101 O. O I I Oyet. OMOMOOMOM0 MMMMM N MMMMMM trnimes011Omisel IS I m Amirmaimoomsimmmsomisim alm:vis . smosi'numemAmmommalemmassimosopmgem -115' 4140 ' Ismistsumulimemammailimmompases ma - im vs. MMMMM mmommem MMMMM pummommosommil .11. mini SOMMOSOOOMMOM.OROMOOOOOO. ISM MO I I kOMO011 M a.O .4 iiiiiIiiill:11:::::a:::;:d1:111!:1 III s s i

1ddlli i . LI,11P1r:Oh::ii:l:r:ffinririllIiililalidaanillklralInMh i III OO mOOMOOM AMOOMOIXOBOOMOOSOO 011.0.01111. .

.. I . PAIVI111:11110111111111111111111111111 ammoommoomm. ...elms.' , alms , a III - s 1101 MOO OSOOOMOOOMOONS MOILONOOMOO MOO 0 Lai 8 mmigemmasskimessemmemimis iOm I I pik1=1:1:11:::::::1111:11:111 I snmil smorommilemmememommom..mmm so LI is: A drillailliiLIMPOIIIN: r i .111:0:11111:11:11:::::::::1::::::111111 II 11 4 t

I I Wiligiiiiiiiiiiiiiiiiiii111111111111 11116 I 4 .411..00mILOOmOOOMMOOMOOOOOm ....1O:.414. I I 11111111910111111151i1111111111531111111 1 II

OP- 0E- OZ. 01 0 01 OZ OE 01, OS 09 I / 1111111111111111111111111111111111111111111 III I 3aisino 111V 31:1111V1d3d1131 - O.

I I 1111111111111111111111111111111111111111 al 1 I

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3unou wnquItl-393 Jemod 3B OOLI VidEl I a 1.

lo - : ': ' ' t e

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I I : : : : ilipintri p;i:::: )..... 4 . s ....:..... A . : ,. ::' =4 ...:::: 2 : 2 1 1 1 : 14 .1::::::i I ... n 3 'kr* ''"1' g4 . n. : : 1 h : 10, .7.47 78 . 1 '6v::::: o p : spivvisporvvv: 3 I 5C 1 3:::. P 3 3 .. 1 1 1 1AtIgag : t;;; .:6411Eggiligr Am. MMg MO PO PPM:nig:di Vgg%, . ,MOMA, 41.41g i 1 .11 N . 1 0.0 xv4 ia. MO l . :: : :44 . . . 44 . ' In . i . !::::4" tp re Se le " gi .... 111411% OP SO." : ..... 0811444144.aigggi 4..v. . 4441 41441444M.V4: ..... NICOCIO, ,g 40r10 ...... cm. ...v ."1118.4.911. .. :11 gligg! 111 vi ...... : . .. ::i g! . ..i ....Mg.." : 1 1 1 ".01a.10 01,... -- .0 _P ...... V ams., I I. wave! .% 4 0:41., " mg SO ." ....vololv4--..6 -ill. 4444"4,04 II .littNI:Hi . . .. i . L. V. is. -4.4 . 1 4 ..- "1111:' 11.4." . - ...... ,..041414.'41414144 II --mime.- t egg' ' .pli00..411,11 . 6:1;7, 1911., " 14 ROO... : siv.- O SE 1 . .:gisivp...... b...... seva:::t1t!;g: , ...... dgi ... V% SO.' .. MD - a .41 p lop 1 1 1 : 6:04::; .. .. . 4444.- Igggillieg0"..09184104144444009 is...... MOP 11014404414 44 GNI :Cr C iv. do._ g 'Am. vlde" : ::: : -- lvv:i Pits... . . ay.._ .4.. I : ..- . :MO :1;SSO' -414149;:ii"lil..... : AV ..OP r-7 MIME 1000 -40-30 -20 -100 10 20 30 405060 16,000 14,000 12,000 10,000 0 10 20 30 0 50 OUTSIDE AIR TEMPERATURE - IC WEIGHT - POUNDS WIND COMPONENT OBSTACLE HEIGHT - KNOTS - FEET (Irv'''. . 1 0

FIGURE95.Takeoff Distance - Flaps Takeoff. 4

I D 11 Yti KNOTS : :

" D I D : - c c- 'ISO CO:osiro:or pug le..:0__._ row 4 Osis000, c 888 i11:8 :::::::: -..SomOOSISS or OM, SOO lolsaillo , oopogoorso: M a 011P MMMMMMMMMMMMMMMM :ISO 0 2OP IIN, OO O . 11. pmPOO8k MSONO 115,00111 11.11. 11,,oOMM. V OM S oo, 1 IL.IIPOSOM : O 011S,o0i I IA, , : EAMIP MO reme,06111 I ,- . I 6 1 .0 1011s Om 1111% 1 041.1410404.414, 1 SoS disc s a tkO :8 A .. litliNes1::!' 1 1 w I, a II e ` c : k mosk6:: . Illiik . 11 kiA i P IIII1.111 .dw memo- ilomp IIIIIIV lir kW.. .,. ,1111011:: 1 'ISOM.- : . MM nos !MU III MMMMM 116 ... .. O: 0, ..... SOO. . Om.MMOIPOOOMP miollc.1110%./OoM 01. . -; ME .ROMILAWOYAMIOAMM.MAILAOOIF.-OO:114 ,...... #*,4eplrel..MIIVOM ,111111* ll'e .10 OromS011.11SO0 '8:1 oo: .-oopool. MMMMMM Om MMMMMM O MOMPOO.MOOMill' mm d 111 els ire ...... a il ...... "40" .% loMOIMI MO MO _coma Om .. 0 .... or di I ow : 6- .- i ..M:SOOO._ :Plilliil ...... !!.. . ;Om!! V.- loom . ossillsOMS..,, , li l .: n oel 0- : :I" B O ...... IN: 1 m . i MO flh a0...... 4O too 0 OOOOOOOOO So.00100olloo 08...:11..., doomill-- ;10 4r0 O110'..50 1 Po6:.,..0oo. - 11;i:d000OC 1:".111!;;; "I "1:!!!;;;ll;rard:180:11:14:tilli I O OOOOOOOOOOO mliwik1. . iv, OOOOOO Mil AukIP OOOOO .. II 11 ; ;le Ie.... or :RI - .1111MiOO 1 -.4 I I: O. Ild:r!::::::: aistie.. 111 11.::::::! ! Nos: 01100loo o osidisioss. - OO10.11dOidiO0:1M411!! Abed. OOOOO odd Amio..momilom00

1 1 1 1 1 :1 111 111 111 1 111 OPERATING CONDITIONS BE-21 BE-22 BE-23 BE-24 BE-25

OAT AT TAKEOFF +10' C 0' C +20' C +25' C -10' C OAT AT CRUISE -20' C -25' C ISA 0' C -40' C AIRPORT PRESS ALTITUDE 2,000 1,000 3,000 4,000 5,000 CRUISE ALTITUDE 16,000 18,000 20,000 14,000 22.000 INITIAL CLIMB WEIGHT 16,600 14,000 15,000 16,000 14,000 ICE VANES RETRACT EXTEND RETRACT RETRACT EXTEND

FIGURE 97.Beech 1900 Climb.

CLIMB- TWO ENGINES - FLAPS UP

MEMEESMINgi MOW - POUNDSCLIMB SPEED - KNOTS MGR MOOMUM Ea= 16200 Off 4'C CONTINUOUS PRESSURE MITTUDE RAPS UP 10,000 11U34 1030 PT WEKiWT 14,000 LES LANDING GEAR UP 1,000 1U 30 124.000 1 RAM OP CLIME 2480 FTAR1 10,000 MD CLIMB GRADIENT 14.7 % CLIMB SPEED. 131 KT$ NOM DURING CP8%431044 241111 CE WINES EXTENDED, RAM OP CLIMB WLL SE REDUCED APPROMOZEIY MO PEST PER MINUTE. 3000

3000

- I 11100I

1000

moo -2

0 -0

400 4 -70 40 40 40 40 40 -100 1020 30 40 50 50 15,00. 14,000 12.000 10,000 OUTSIDE MR TEMPERATURE- WEIGHT - POUNDS

FIGURE 98.Climb - Two Engines - Flaps Up.

278 84 - 111 : . III rrr -; rrr rrr III : a

- ---I

0 01 UV rrr OOOOOO 1911 OW/ OO /1111. I 111/ OOOOO TT OOOOO a...... 1 ...... " . o." "re"r0 "". ..*" . ..11 ... '': . gri:: ,r,., rr . . ,19 " LiAtliiitro ::#:::70 . .19. :01:%::: r4-, ...0 .....:: . ::' "II," 1 ..... R'r'-'1 ::,41::711::%:::::0::7::7' ;II 3 ,041 TV"" 6:::::: . ::: ...... rr I o, OOOOO 11.. ,.j:::". ". .." aroe ...... ! . . .. so 06 ... 1 .44,M Afta .6vVIO ...... rr ...... di.;;;V; OOOOOOO OOOOO i o " I .... '" ". . ,f :::. P a1919.... 411 "...... / OOOOO WO Alf ..... 'to si

ir OOOOOOOOOOO 00,1,11,

"WE MIO00 I o

AII -- INIIIME IMIMME I ; I I Al I rl ;III I I III I11,1 C '': Olt

I - 1 1 I I1 1 1 I 111 I I I 1 I 1 I 1 I III

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I 1 ; ..... I I I I I I I I . ... . =IMM 11 11 11 11 /1

II Appendix 3

OPERATING CONDITIONS BE-26 BE-27 BE-28 BE-29 BE-30

OAT AT MEA -8*C+30°C +5°C+18°C+22C WEIGHT 15,500 16,600 16,000 16,300 14,500 ROUTE SEGMENT MEA 6,000 5,500 9,000 7,000 9,500 b:" BLEED AIR ON ONI OFF ON OFF

FIGURE 101.Beech 1900 Service Ceiling.

OPERATING CONDITIONS BE-31 BE-32 BE-33 BE-34 BE-35

WEIGHT 15,000 14,000 13,000 16,000 11,000 PRESSURE ALTITUDE 22,000 17,000 20,000 23,000 14,000 TEMPERATURE (OAT) -19' C -19' C -35* C -3V C -3' C TRUE COURSE 110 270 185 020 305 WIND 180/30020/35135/45340/25040/50 CRUISE DISTANCE 280 320 400 230 300

FIGURE 102.Beech 1900 Cruise.

87 283 Appendix 3 Al11i6.- SERVICE CEIUNG ONE ENGINE INOPERATIVE BLEED AIR ON BLEED AIR OFF

0 AO 70 40 40 40 40 40 -V0 70 00 U AO AO 40-70 40 40 40 41 40 0 0 10 0000 AO 00 OUTFIOE AM TEMPERA/URI - 'C OUT= AIR TOPERVUEE -'C SERVICE CEIUNG . MAXIMUM ALTITUDE FOR 50 ft/min RATE OF CLIMB

FIGURE 103.Service Ceiling - One Engine inoperative.

284

88 RECOMMENDED CRUISE POWER

1550 RPM

ISA +10°C

WEIGHT 16,000 POUNDS 14,000 POUNDS 12,000 POUNDS 10,000 POUNDS

TONOUE FUEL TOTAL TONGUE FUEL TOTAL TONOLIE FUEL TOTAL TONGUE FUEL TOTAL PRESSURE*OATOAT PEN PLOW PUP. IASTAE PEN PLOW FUEL IASTAE PIE PLOW FUEL IASTM PEN PLOW PUEL IASTAE ALTITUDE ENO PIN PLOW ENO PEN FLOW ENO PEN FLOW ONO PEN FLOW ENO ENO ENO ENO

KTSKTS FEET CC PT4.11111 1.10/101 LSVINIKTSKTS FT-LIIS INS/NNLW OWNTSPITS PT4J$ IMAM LES/1411 KTSNTSFT-Up MOIR U1S/161

SL 3025 3294 577 11542322393301 577 1154235241 3307 577 11542372433312 577 1154238245

2000 26 21 3191 551 11022272403198 551 1102230243 3204 552 1104232245 3209 552 1104233247

4000 22 17 3092 527 1054222242 3100 528 10562242443106 528 1056227247 3111 528 1056228249

6000 19 13 2992 504 10082162433000 505 10102192463006 505 1010222249 3012 505 1010224251

8000 15 9 2886 481 9622112442896 482 964214247 2903 482 9642162502909 482 964219253

10,000 11 5 2778 458 918 2052442789 458 916208248 2797 459 918211252 2804 459 918213254

12,000 7 1 2636 432 864 1982432648 433 8662022482657 433 8662052522664 434 868207255

14,000 3-32495 408 816 190241 2508 409 818195247 2518 409 818198251 2525 409 818201255

16,000 -1 -7 2352 384 7681822392367 385 770188246 2378 385 770 192251 2386 386 772195255

18,000 -6-11 2208 361 722 1742352226 382 724180243 2239 363 726 1852502248 383 726188254

20,000-10-15 2063 338 6781642292085 340 680172240 2100 341 682 177248 2111 341 882181153

22,000-14-19 1911 318 832 153221 1939 31/ 634183235 1957 319 638169245 1969 319 638174252

24,000-19-23 1749 292 584 1372061790 295 590152229 1812 297 594161241 1827 298 596167249

25,000-21-25 1649 279 558 1221871714 284 588147224 1739 286 572156238 1756 287 574183248 /

FIGURE 104.Recommended Cruise Power - ISA +10' C. 286 285 RECOMMENDED CRUISE POWER

15:.00 RPM

ISA

WEIGHT 16,000 POUNDS 14,000 POUNDS 12,000 POUNDS 10,000 POUNDS

TOSOUI FURL TOTAL TOROUI FUEL TOTAL TOSOUE MIL TOTAL TORQUE PURL TOTAL PREMISSPATOAT PIE PLOW POD. LAS TAI PIE PLOW FUN. LAS TAI PRE FLOW FUEL MSTAP PIE PLOW PURL IASTA! ALTITUDE ENO PIE PLOW ENO PIE PLOW MO PIE PLOW INS PIE PLOW MO ENO IWO Ella

UItT CCPT-LIS LSS/KE MANIITSITSPT-UIS Lame LAWNSITSITSPT -LaLIMO LIPS/H11 ITSITSPT-LIS LIMPID LIMEITSITS SI- 20153400 586 11722372393400 585 1170239241 3400 585 11702412433400 585 1170242244 2000 1711 3400 573 11482342443400 573 11482382483400 572 11442382483400 572 1144240249

4000 13 7 3400 560 11202322483400 559 11182342503400 559 11182362523400 559 1118237254

8000 9 3 3397 548 10962292523400 548 10962312553400 547 10942332573400 547 1094235259

8000 5 -1 3253 521 10422232533260 522 10442252563265 522 10442282583270 522 1044229260

10.000 1 -53092 494 9882162523100 494 9882192563107 495 9902212583112 495 990223261 12,000 -3 -92929 466 932208251 2937 467 9342122552945 487 9342142582950 467 934217261 14,000 -7 -132772 440 $802012502781 441 8822052552789 441 8822082582795 442 884210261 16,000-11-172808 414 8281932482818 414 8281972532628 415 8302012582833 415 8302113281

18,000-15-21 2435 388 7761842442449 389 778189251 2459 389 7781932582487 390 780196280 20,000-19 -252283 363 7281152392282 364 7281812482294 365 7301862542302 365 730189259 22,000-24-292094 338 6761842332118 340 6801722442133 341 8821782512144r342 684182257

24,000-28-331931 315 630152223 1980 317 634163238 1979 318 d36189248 1991 319 838174255

25,000-30-35 1846 303 8061452161880 305 810157235 1901 307 614 16524611,1 308 616170253 287 88

FIGURE 105.Recommended Cruise Power - ISA. RECOMMENDED CRUISE POWER

1550 RPM

ISA -10°C

WEIGHT 16,000 POUNDS 14,000 POUNDS 12,000 POUNDS 10,000 POUNDS

TONOUE FUEL TOTAL TOME FUEL TOTAL TOROUE PAL TOTAL TONOUI MIL TOTAL PRISSURE,IOATOAT KR PLOW PULL URTAI MR FLOW FUEL IASTAE PER PLOW FUEL URTAE PEA PLOW PULL IASTEl ALT/TIJO, IRO PER PLOW ENO PER PLOW ENO PM FLOW ENO PEN PLOW MO INS KM INC

PUT CC FT-UIS LSSA411 ~IRKT,ITS FT-LIIS LIMN IJSRUIKT,ITS FTLOS Luneus/NnVSITS FT-1.1111 LURIA LIS/RRKTSKTS

SL 10 53400 582 1164238237 3400 582 1164240239 3400 561 11822422403400 581 1162243242

2000 8 1 3400 569 1138236241 3400 569 1138238243 3400 568 11362402453400 568 1136241248

4000 3 -33400 558 1118233245 3400 557 1114238248 3400 557 11142372493400 557 1114239251

6000 -1 -73400 548 1096 2312503400 547 1094233252 3400 547 10942352543400 546 1092236258

8000 -5-11 3400 538 10762282543400 538 1076231257 3400 538 10762322595400 537 1074234261

10,000 -9-153400 530 10602262593400 530 1080228282 3400 530 10602302643400 529 1058232266

12,000-13-193200 499 9982182583208 500 1000221281 3215 500 10002232643220 501 1002225268

14,000-17-233010 470 9402102563019 471 942213260 3026 471 9422162633032 472 944218266

16,000-21-272823 442 884202254 2833 442 884205258 2841 443 8662092822848 443 886211265

18,000-25-31 2641 414 82P 193251 2652 415 830198256 2661 416 832201261 2668 :16 832204264

20,000-29-352456 387 774 184247 2471 388 776189254 2481 389 778 1932592489 390 780196263

22,000-33-392277 361 722 174242 2298 363 726181250 2308 383 726 1852562318 364 728189261

24,000-37-432105 336 872 1632342128 338 6761722462144 339 678 1772542155 340 880181260

25,000-40-452017 324 846 157230 2044 326 852187243 2061 327 6541732522073 328 656177258

FIGURE 106.Recommended Cruise Power - ISA -106 C. 289 290 3

I I 4 . - I I

. 4 II . II 3 3 I . lit 4 I I.N33030 '0331:13 003 SJ.ONN

III

OOOOO III IT :111,

I 4111 O I 1111, 4011ION111 SIM OOOOOOOOO III1IIIII1I 1f, WWI OOOO r . OOOOOOOO la IMI S I/I II Ueda 'MMMMM I IMMO OOOOOOOO IWr BIM IM S II SIMMS OOOOO 1115 13JI 11111 MEW OOOOO ID UM OOOOO Ulla IL dein sm. ems also a a SEW I OOOOOO 1 1111111 O II 1111.111 .or.1411.11, as.... 1 I OOOOOOOOOO 11111 111111M1111111111111111

namul=mit

11 - II I . ammo noulms I I

3 t Appendix 3

OPERATING CONDITIONS B-38 B-37 6-38 6-39 6-40

PRESSURE ALTITUDE SL 1,000 2,000 4,000 5,000 TEMPERATURE (OAT) +30' C+18' C 0' C+20' C ISA WEIGHT 16,000 14,500 13,500 15,000 12,500 WIND COMPONENT (KTS) 20 HW 10 1W 15 HW 5 1W 25 HW RUNWAY LENGTHFry 4,000 4,500 3,800 5,000 4,000

FIGURE 108.Beech 1900 Landing.

292 93 NORMAL LANDING DISTANCE-FLAPS LANDING ANTI-SKID ON ASSOCIATED CONDITIONS: EXAMPLE: POWER REDO) TO MAINTAIN SOO FTIMIN CAT ON FINAL APPROACH 25C RUMPS' PRESSURE ALTITUDE 5995 FT MED, LEVEL, DRY SURFACE LANDING WEIGHT APPROACH SPEED IAS AS TABULATED 14,152 LEIS HEADWIND COMPONENT 10 KTS BRAME) MAXIMUM 112.2 GROUND ROLL 1150 FT TOTAL OVER 50FT OBSTACLE 2195 FT APPROACH SPEED 109 KT'S 3500 C ::

6 1;11 Ti Ti I o 0000000 DOOMED.' 3000 : Ti.-- II :loonggs::: tf 000000 m 7 ::::

r, I PO ::

; .41 Is ill! 11 311:::::!: mm : :::: 11: One ,11411::4 Ag0 111111 EMI MuSOMOOD.4211 OW. m :11 !: : :::::Osoo:00000000000000 go rat 00000 DOM OF/ , nn a 2 A ' wAt t! 4Oule 1 :am A: :11 t' 1 11 Ati:ri::1 : qiiiiiiiiiiii : Pi.:1:Viliii: ilVer; Alii:Nbil : : AIIIII Irsi:ilivi lig ::::::1;:iiir i rm. : ! worn' ,4.... .41.4liggi I lq4 um . oo ellq.v. o I ::soolt;144 'ORmAI:244::11 Minn eNtball : 411:;;;!1::::gosossl OOPOWKW Ii.oggeng.-.00.songn 000000000000 :MN: P10011._ I. oU60.1.61b .:::1115i!ii!:114:iiiel 0.1:;;ig::!!,..- .--.0.. _.. 00S. sr l 1 41;.t. : 'noso.no. O onlr:::: , 8..-Ipi66;:!"-nt ..:"::;; 6;.:2"."' aii Ann's. mgOwsil 4 a 0I O 00n.n. o."_.:!Iiii;!!!- .. , Airan WO..-.. 00000 . .1114.- .. t .II, :::4100:4 a 00000 _ 4 oo 00000000 ... .1 wig, 6. , r . t i U. ::::;11. .. 0000000 '- ra,.:!:::!i2:::::Sg. esottril: %fa 1!::...... tilseam..1.110111 ORMM,4 00000 amp; :rim:D o O. .0011. !1% 000000 4Dges..-.11 , Volg 10111. .m0m100. .mmar. m 000000 ones, 111 fi D.. -..014011010. .1110ii. 1:%;:,011114MOMO.MOOO ND o OND;O:illii : ii 4;::41::::;0;:4t:::S' gi..00;0.,.. 'minim._ .:110.:gs. . 0 ..t, 0.4:::11:1.4 one , t 00000 :gnosis.- *maMIS i i ;:24:1 1 ._ rAmph.'' I I -mmm:O ooo.01.11:11 I :1iMrZ o ,ADSOMOSMOO1 i ;..:mmmmm MIMMIIMMINIIMIMENNI I -.. - 14,000 12,000 10,000 0 10 20 30 0 50 OUTSIDE AIR IF IPERATURE WEIGHT - POUNDS WIND COMPONENT OBSTACLE HEIGHT - KNOTS - FEET

FIGURE 109. NormalLanding Distance -Flaps Landing. ._i_. illilgiiillie 4Nktimikkil,._ _.... 10\4Z.VAilis4'.ggi_'M'I' 19 1 Iliiiini1p4 1 IlC MSNiddili*.,*MOK1 Ilk I 11111E0VisiMINAMMEI 1LM1OOLV A' 0k. - A.. 111111110MMIMISSMNNE 111:11111Newi IN Sm.__ 1 1 111:11470 1 1.- . ....s. la 1.11:11.41:tikl ZlikilUIL L-11 1 *, - g:13:132"11 ` iftwala '111-li , 1 1 1% ,e 21:r1 -11ohk, 1,sh_ 1174, IAA. 9. _... 11116:s 1.. ...,,ilgtsigg 1 11 1 ... 5i NIT li Iiiillild§11, AA'', 110...A.N. C.hahlikgol, Eli IMINFgilln 1 .1 ,Nle1 ii q .'I r" . . L ika NIMkgPN ML --.. . ."6.

295 FIGURE110.Power Assurance Check. 296 HOVER CEILING IN GROUND EFFECT 0° TO 52°C MAXIMUM CONTINUOUS POWER SKID HEIGHT 5 FEET ENGINE RPM 100% HEATER OFF GENERATOR 400 AMPS ENGINE AND ENGINE INLET ANTI-ICE OFF

14,004 FT. DEN. ALT. LIMIT

maw MAX. DEN. ALT. imehmANDG.'N. LIMIT

% KIMOAT °C /111 11111A1? Bi OIL VI II AM MAX.OAT ow loi PAAUVA AIM PLIN AMY MI AEI IMIIIIIll IMMIXAIWA MOW NUMMI 131 EPA 1'

MAX. GROSS- !INMI WEIGHTLIMIT tk.

0 10 20 30 40 50 60 10 11 12 13 1415 16 17 18 OAT °C GROSS WEIGHT LBS x 1000

FIGURE 111 .Hovering Ceiling- In Ground Effect.

296 c

il c I I I

I , c II c 'A'

IAI c

: .

_ I , s c III

c I II TAKE-OFF DISTANCE OVER 50 FOOTOBSTACLE 521TO -35C INITIATED FROM C. FT. SKID HEIGHT HOVER POWER + 10% TORQUE VTOCS= 50 KIAS ENGINE RPM 100% HEATER ON OR OFF GENERATOR 400 AMPS ENGINE AND ENGINE INLET ANTI-ICE OFF

14.000 FT. DEN. ALT. LIMIT

0%. NOTE MAX. DEN. MINIMUM OPERATING TEMP ALT. AND AUT'ORIZED TO -35 C G.W. LIMIT

MAX. OAT

INIF AU111111111 IIVAN 111111111=11111111 U/ /y 11111 sommusimml Ilia III IIIMMLIMGROSS WEIGHT- LB. 10.000 MN IINUMME 11.000 12,000 111/IIMMEZ 13.000

MIA II IIIMINANS 1514.00°,000 16.000 IWO II IHKANftli17,000 11/1 IBM 4144 117,500 MU INN11061111 -60 -40 -20 0 20 40 60 800 800 100012001400 OAT - °C TAKE-OFF DISTANCE- FT.

FIGURE 113.Takeoff Distance Over 50-Foot Obstacle.

299 es impunimommosmimmommommuili AppindIx 3

..112 KIAS IIFR):, INN

I. i .1 NOTE: WITH NEATER ON ABOVE 11100 FT.. RATE OF MOO CLIMB III 310 FT./MIN.LESSit._

1- I- - i -11 r--r- .1 .. ENGINE RPM 100% - 1 GENERATOR 400 AMPS .1 j. GW 16,000 LBS =110.1M111a NOTE

Iv MINIMUM OPERATING ! TEMP.AUTHORIZED 10 -35 'C

S . ;. _.4_00.000

; 8.000 ; 1"

MAX 1 OAT 2.000

. . 6 - .1. 1 . 101 114".. L I I i- RATE OF CLIMB...FT./PA N.3t 1001j. I i I _ ! f I TWin engine maximum continuous power climb performance IFR engine & engine inlet anti-ice off heater off 100% NR 16,000 Lb. G.W.

FIGURE 114.Twin-Engine Climb Performance.

99 300 k 1

1 1 1

NHL `11,1/L IRM I INV' MINN Min 0211 1113111, Onas 11 EMIS11.1511111 Ell 111 -0 Aim In MILLINE.1110110 WIN 11 Ailti IMMO 11111111111 kt;q1-11111k, k*111 MINIS nal.1 1, Imo nor"! _r_u_a!/71-77.17AterN 1111111111111 %MEM

I I. 1 1 ,

. 1 1 C

1 1 AIRSPE f D I IIVIIT`04,NrI KIAS 1--.5500 LB AiRsPf-fD LIMIT kVNE) ,KIAS PHI ,-,,, Al 1 IT-5(104C0 '-i 1)AT 1 : PHI (0-, Al F ,F T X1000 i H 1, 16 1H 20 1, kl::%, . 2tt ( 4 1 /, 4i) .1

135.00 LB AlF1',PF f D IIIV46T NE Kr."0, r16500 l E3 AIHtit fE t1t IMITvNti h A

C) /1.1 rrl '.j! :1 4.

'175(10 LR Alf`,1'1 tl I I"\...1'",.Nif 1 4-14500 L6 AIII(WE I L KlAk, r km Hi Ai .` A

1 .11

'_:FAM 1111111111W/W IIIIIVNAVANIMII- Ilez),:Amis mowAu 111111`-allIIIIIINAMEM11111 16;IVAIImmENENNIII Er:All 1110111/11 AMU 11111fibiAltall IIMEMIMME I/I ENNEINAMIll NM;111E111611111 AU VIINAMEMIIIII 1111WE Aril Elerill1111 IIIfi MAIIfinglAnon III III/ IA MICIWARS! SOO . ... ME AtNOMMES1 ... VIII; MISAVASER .110 MINVIIIIIIM IMF.aMEN1111111111

11101W-111 MEIJI I It II MIMI .6- I IMF III IfilA1111111111111111 1 1 .1 1 1 1 1 1

C 11

I I/ 111 _ 11o. 1

111:qii!111iiiiNi1111111111111111111111111f111111:1ffilli111111m1

1-1 ."1111i,!".11.1111111011111111111111111 .11111111111111111111111111111111;::::11fliimi111111111 111

1 11111011111111iiimm.sii111i'111,il!,11111illiii1111N111111111111'.111111111iii. 11'111111111111 11

MN;11111111111111,11111 111.1:"941111111Rilii;11111111111111111:: 11

111111111Nih,:;i: :9'dill' t1111111e ,1111111111111i11111111110ii, ,,I111111 11

.1 111111111 11111E111 1141,11Pitail:.,.111111111iii.11111:11111111111N1111111111111101411:1!:1;;11 U

1 11110111 1111111mm II 411,1P,1111114'iS111111111111111r1(1111111111, 11111111W:.1VIUtU 11

Him H11111111111i111 ,11111116;;Ii1111';11111111;',91111TalliiirilliIIIIIM111111191iii !!

:1 _ [1111111 11111111it1 iir,111011111111;011111111P;I:!11111111111141IEW111111 111:1111 H

11114 11H11161,11111111r,11111111111,4111111111 ":11111111L 11111111111111111111M:!111 1111111I 11

111111militiii1:1;11111111r:11111;1111111 1111;,,"11111111::411111111011111111i! HIM 11

11111111 111111111 11111111111111mi11:,11111111"11;1: '111111111M1111W11111111101111,1111 II

11111111 1111mi,i11111111:11111111',1H101111,,11111, 11111111111k:11111111111:1111g01111 1111111II!

11111111 1111111 11111111111111K11111111111111111.,m .1.1110,1111111!111!!!1;11:11111111111111 11111111 I

111lim111i11 u1i111,1111111,111111114;;;11411111110:11,11111111:1111.1110111M11,111111111i11 1111 III I i1 11111111 1111111111,:ii1111111;1111;;11111111:',',1111111"011.:iiii11,11111111101111111h,11111111i4 1111 I1H 1

1111111Ilir1111;,111,1411111:1 ,11111111111,11r...i 11:1111 111011111M711111M11111 !III HI M

11 1111111111,1111,111,g1111,!: 1;111111,1111111111:4 111111i11,!Ji 101111110 11111111'111M 1111111 I m 11111111 11,111,f1I.'ir1Vilq:111!!11i11:1111111.11. 11111111:111111111.11111.111111111111moiuii I Ilr 111:1151P, ,1111,211111:111111.11011111611111111 11::::1.11 III' IllIII

11H1111 it:P1M11101111111.11riiii 100111 111111111, 111115111111111111111 1111 III II

11 MI ill Mi'imm11111111m11111111.1 1111011101 "111111111111111111111111111 1111 111 I

6 11111111 11;1:1.111; 11111.11.min itimmlr 1111 111 1

1111[111111)":1 :11 i'l'.1:1,1,1.11111ilitimil'it..!!!1111111111"111'111 141111111111111111111111111111Hullili1111111hr11111 1111 HI I

1111111 Wili:1i! 1;1 ,Ifii111111,01iiI1111.1,11,1111111,111111 11111111111111111111 11111111 HI

1 111111 1 inon::111; 11111111i;,..:11;1111m1 111111,Mlii ,Ilm If! III 1 111111111 1 imr.mmiglimi:::111111111mmr" H mug Ai imm111

1111111111 1 IIIHM1111111M11111111M1111111111111111 111111111111111 umum1111_111011111 1111 HI I mintgisillinll I 11111 1111illtIll 1111111111111111111111111 BM liltIIIill

FIGURE118.Wind Component Chart.

103 304 " I " OgItIZIF T II

INCREASING INCREASING HEADWIND TAILWIND

-e2of3/ 4 4° -410 OUTFLOW 1111111511w OUTFLOW '410P Age..- 1111111...

TYPICALLY S. tp2 MILES

FIGURE 119.Miaeburst Section Chart. 306 305 Appendix 3

SURFACE AVIATION WEATHER REPORT

AUS SA 1753 40 SCT E250 BEN 6 170/87/60/1911017/006 BPT SA 1755 30 SCT E250 BKN 7 183/93/74/1704/007 BRO 8A 1/55 34 SCT 250 -OVC 6H 183/93/74/1415/001 CDS SA 1758 E18 OVC 7RW- 183/73/69/1113/012/RW+ E-S BINOVC R8211 CU. SA 1749 30 SOT 250 -BKN 7 161/93/89/2111/008 COT SA 1749 40 SCT 200 SCT 10 160/87/70/1310/002 CRP SA 1753 28 SCT E250 BKN 10189/90/75/1616 /003 DAL SA 1755 23 SOT E100 OVC 7 87/71/1605/007/HLYR DFW SA 1810 35 SCT E120 OVC 10 174/85/68/1707/008 DHT RS 1756 E25 BKN 16 200/72/59/0414/026 DRT SA 1756 20 SOT E100 BEN 250 OVC 10 145/82/72/1212/00 0 ELP SA 1755 70 SCT 250 SCT 60 131/64/56/0907/015 FTW SA 1750 25 -SOT E100 OVC 7 84/68/1807/008 FTW UA /OV DFW 180005/TM 1803/FL095/TP PA30/SK 036 OVC 060/070 OVC 0 75/0VC ABV OGG SA 1745 250 SCT 15 89/139/1508/011 MA BA 1755 25 OCT E200 BEN 7 92/71 018 SP 1811 AMOS 88/74/1705/007/000 HOU SA 1752 30 SCT E250 OVC 7 80/70/1506/008 HRL SA 1753 E250 OVC 7 93172/1415/002/ FEW CU E IAH SA 1755 33 SCT E250 BKN 10 161/87/73/1207/007 INK SA 1755 E30 BKN 60 BKN 250 BKN 20 144/81/61/0406/088 LBB SA 1750 E12 BEN 30 BKN 100 BEN 12184/70/67/04'3 /015/ RB15E40 LBB SP 181815 SOT E30 BKN 100 BKN 12 0412/015 L88 UA /OV LBB 045002/TM 1821/FL060/TP13727/SK 045 BKN 0/53 TOPS RGD LFK SA 1756 300 -BKN 7182/01/66/2407 /008 MAF SA 1756 M25 BKN 250 OVC 12 142/80/64/0220/009 RWU E-S MFE SA 1756 250 -BKN 7151/92/86/1315 /998 MRF SA 1752 AMOS E30 8KN 60 125/81/57/0912/000/ PK WND 20 MRF SP 1811 AMOS 83/58/0809/000 PK WND 20

Ravi% 120.Surface Aviation Weather Report.

307

105 SURFACE AVIATION WEATHER REPORT

MWL SA 1758 Ell BKN 50 OVC 10 E189/77/73/1311/008 PSX SA 1755 18 SCT E200 OVC 7 183/87/78/2010/007 PVW SA 1750 12 SCT E30 OVC 10 185/85/88/0508/011/ BINOVCNE SAT SA 1758 28 SCT E250 OVC 7 184/85/89/1518/005/UA /OV SAT TM 1739/FL UNKN/TP UNKN/SK TOPS 040 SJT SA 1755 E18 BKN 70 OVC 7 170/77/72/2212/002 SPS RS 1757 9 SCT M25 OVC 8R- 185/75/71/0914/011 SPS SP 1820 M15 OVC OR- 1010/011 SPS UA /0V SPS/TM 1815/FL090/TP C402/SK OVC 050-080 TPL SA 1751 15 SCT 100 SCT 250 -OVC 15 89/89/1715/007 VCT SA 1755 30 SCT E250 OVC 7 179/88/73/1713/005 AR ELD SA 1755 250 -BKN 6H 190/88/70/0805/010 FSM SA 1758 E80 BKN 120 OVC 20 191/88/89/2805/011 FSM UA /OV HRO-FSM/TM 1825/FL290/TP B737/RM SCT TOPS 290 FYV SA 1755 35 SCT E80 BKN 250 OVC 15 202/83/70/1705/016 / RWUSE HOT SA 1751 40 SCT E150 OVC 15 91/82/3408/010 HRO RS 1755 20 SCT E35 BKN 13T 195/84/72/3007/015/ TB30S-SSW MOVG E RN THDR HRO SP 1825 E15 BKN 35 BKN 13TRW- 1810G20/018/ T SE-W MOVGNE LTGICG RB25 UT SA 1754 30 SCT E250 BKN 10 182/93/89/0704/007 PBF SA 1753 40 SCT E100 BKN 5H E183/95/68/2907/007 TM SA 1753 10 0 SCT 200 -BKN 7 92/88/2503/010

FIGURE 121.Surface Aviation Weather Report.

308 108 Appendix 3

TERMINAL FORECAST

AU FT 031515 C12 BKN OH 1415.17Z 030 BKN 1515025. 19Z 40SCT 0250 BKN 1515325 SLGT CHC C20 BKN 3TRW. 01z 150 SCT 1315. 07Z C8 BKN. 09Z IFR CIG. 14Z MVFRCIG.. AIM FT 031515 C10 BKN 80 BKN 0512 OCNL C10 OVC 2TRW+. 18Z C20 BKN 80 OVC 0315 OCNL C10 OVC 2TRW+. 14Z C10 OVC 5R-F 0312. 09Z IFR CIO R F.. AUS FT COR 031615 1545 C25 BKN 100 OVC 1710. 18Z C30 BKN 100OVC 1710 CHC C10 OVC117-1W. 04Z C14 BKN CHC C10 OVC 1TRW. 09Z MVFR CIG TRW.. BPT FT 031515 25 SCT 8H. 17Z 30 SCT 250 SCT 1810. 01Z 250SCT. 09Z VFR. 10Z MVFR FK.. CRP FT 031515 20 SCT C250 BKN 1515025. 18Z 30 SCT C250 BKN1615325 SLGT CHC TRW. 01Z 150 SCT 1815. 09Z VFR.. DAL FT 031515 30 SCT C100 BKN. 17Z C30 MN 100 OVC CHC C10 OVC 2TRW.01Z C20 BKN CHC 3TRW. 09Z MVFR 00 TRW.. DRT FT AMD 1 031515 1520Z C14 OVC 1410. 18Z C20 BKN 100 OVC 1410CHC 3TRW. 19Z C30 BKN 100 BKN 1412 CHC C20 BKN 3TRW. 02Z 35 SCT C80 BKN CHC C20 BKN 3TRW. 09ZMVFR CIG TRW.. ELP FT 031515 70 SCT 100 SCT. 17Z 70 SCT C120 BKN 0812 CHC 050 BKN5TRW G35. 08Z C70 BKN 0712 SLOT CHC RW-. 09Z MVFR CM.. HOU FT 031515 20 SCT OH. 17Z 35 SCT 250 SCT 1810. 01Z 250 SCT. 09ZVFR. 11Z MVFR FK. IAH FT 031515 20 SCT 8H. 17Z 35 SCT 250 SCT 1810. 01Z 250 SCT. 09ZVFR. 11Z MVFR FK.. INK FT 031515 20 SCT 100 SC! 1010. 182 C25 BKN 80 BKN 0813 CHC C10OVC 1TRW+A G35. 04Z C20 BKN 50 OVC 0513 OCNL C10 OVC 1TRW+. 09Z MVFR CIG R F. 11Z IFRCIO R F.. U3B FT 031515 Cu 0 BKN 50 OVC 0812 CHC 10 SOT C20 OVC 3TRW. 17Z C20BKN 60 OVC 0415 OCNL C10 OVC 1TRW+. 04Z 010 OVC 4R-F OCNL 1TRW+. 09Z IFR CIG R F.. SAT FT 031515 C16 BKN 8H 1710. 17Z C25 BKN 1715. 19Z C30 BKN 250OVC 1715 CHC C20 BKN 3TRW. 05Z C14 BKN CHC 3TRW. 09Z MVFR C10 TRW.. SJT FT 031115 C15 BKN 50 OVC 1210 OCNL 03 OVC 4TRW. 20Z C25BKN 70 OVC 0912 OCNL C8 OVC 1TRY+ 09Z IFR aa R F.. SPS FT 031515 30 SCT C80 BKN 0712 CHC C10 OVC 2TRW. 09ZMVFR CIG TRW..

FIGURE 122.-Terminal Fcatluce.I.

309 107 AREA FORECAST

DFWH FA 031040 HAZARDS VALID UNTIL 032300 OK TX AR LA TN MS AL AND CSTL WTRS FLT PRCTNS...IFR...OK TX ...MTN OBSCN...TN AL ...TSTMS...OK AR TN AL

TSTMS IMPLY PSBL SVR OR OTR TURBCSVR ICG AND LLWS NON MSL HOTS NOTED BY AGL OR CIG THIS FA ISSUANCE INCORPORATES THE FOLLOWINGAIRMETS STILL IN EFFECT...NONE

DFWS FA 031040 SYNOPSIS VAUD UNTIL 040500 AT 11Z STNRY FNT ALG LOU MEM ABI MRFLN. LGT MOIST NELY LOW LVL FLOW N OF FNT. S OF FNT MDT SELY LOW LVL FLOW FM GLF OVR TXAND LOT WNDS ELSW. LTL CHG IN SYNOPTIC PATTERN THRU PD.

DFWI FA 031040 ICING AND FRZLVL VALID UNTIL 03230 0 NO SGFNT ICING EXPCD OUTSIDE CNVTV ACTVTY. FRZLVL 130 N PTN TO 180 S PTN OF AREA.

DFWT FA 031040 TURBC VALID UNTIL 03230 0 NO SGFNT TURBC EXPCD OUTSIDE CNVTV ACTVTY.

DFWC FA 031040 SGFNT CLOUD AND WX VALIDUNTIL 03230 0...OTLK 03230 0-04050 0 IFR...TX OK FM LAR TO OSW TO SAT TO MAF TO LAR CIGS BLO 10 VSBYS AOB 3F. CONDS IMPVGAFT 19Z. MTN OBSCN...TN AL FM BML TO AGS TO BMH TO LOZ TO BML MTNS ERN TN AND NERN AL OCNLY OBSCDIN CLDS AND PCPN. TX OA N OF ROW MAF SAT OSW LN GIGS BLO 10 VSBYS AOB 3F WITH MEGG LYRSTO ABV 240. WDLY SCT LGT RAIN. CONDS BCMG BY 19Z CIGS 15-25 BKN-OVC AND MEGG LYRS TOABV 240 WITH SCT LGT RAIN AND WDLY SCT EMBDD RSHWRS. RSHWRS BCMG TSHWRS 17Z-23Z. CB TOPSTO 350. OTLK...MVFR CIGS F TRW BCMG IFR CIG BY 05Z.

RMNDR TX VSBYS 3-5H ERN PTN AND OCNL CIGS 10-30OVC 50 MSTLY CNTRL PTN. AFT 17Z CONDS BCMG CU 30-40 SCT-BKN 100. OTLK...MVFRCIG TRW. RMNDR OK AR EXTRM WRN TN ONLY 90 OVC WITH MEGG LYRS TO 160 EXCPOCNL CIGS 15-25 OVC IN SCT TRW-. CB TOPS TO 350. OTLK...MVFR CIG TRW.

FIGURE 123.Area Forecast.

1083 1 0

...... Appendix 3

CONVECTIVE SIGMET

MKCC WST 031755 CONVECTIVE SIGMET 42C VALID UNTIL 1955Z TX OK FROM SW MLC-PEO-SJT-5W MLC AREA SCT EMBDD TSTMS MOVG LTL. TOPS 300. CONVECTIVE SIGMET 43C VAUD UNTIL 1955Z CO KS OK FROM AKO-OSW-30WNW OKC-AKO AREA SCT TSTMS OCNLY EMBDD MOVG FROM 3220. TOPS 380. CONVECTIVE SIGMET 44C VALID UNTIL 1955Z 50NE MEM MOLD INTSD LVL5 TSTM DIAM 10 MOVG FROM 2825. TOP ABV 450. OUTLOOK VALID UNTIL 2355Z TSTMS OVR TX AND SE OK WL MOV SEWD 15 KTS. TSTMS OVR CO, KS, AND N OK WL CONT MOVG SEWD 20 KTS. TSTM OVR TN WL CONT MOVG EWD 25 KTS.

FIGURE 124.--Convective SIgmet.

311 '''109 WINDS AND 1 ,IvsPERATURES ALOFT FORECAST

DATA BASED ON 031200Z VALID 040000Z FOR USE 1800- 0300Z. TEMPS NEG ABV 24000

FT 3000 6000 9000 12000 18000 24000 30000 34000 39000 ABI 1306+16 1607+11 1807+06 2108-072208-18240833 250942 300753 ABO 0810+14 0511+08 3415-063220-18 312333 312543 302554 AMA 0614 0814+10 0709+05 3210-072914-19 281934 282243 292554 ATL 0906 9900 +17 9900 +12 0205 +07 3507-073305-19290534 280543 990054 BNA 9900 9900+17 3205+12 3109+07 3018-072918-19 272134 262444 262855 k BRO 1510 1614+20 1611+14 1708+08 9900-079900-19990034 990043 990055 DAL 0910 1706+17 2009+11 2011+06 2015-082214-19 231333 241342 271153 DEN 9900+09 9900+04 3020-103029-21 303636 304145 294756 DM 3615 3315+07 3118+04 3022 +00 2835-12 2748-24 276438 277348 277957 ELP 0810 0614 +13 0815+08 0113-053614-17 361433 361442 251354 C3CK 0611+11 0809 +08 9900 +03 2817-092823-20 273135 273844 284155 HLC 0409+09 0405+07 3106+02 2822-10 2730-21 273936 274545 275256 HOU 0909 1807+19 1606+13 1606+07 1605-089900-20990034 990043 990054 ICT 0516 0813+12 0607+08 9900+04 2718-092626-20 263635 264144 274655 IND 3811 3207+12 2912+08 2818+03 2733-09 2643-21 265835 265944 256255 INK 0809+18 0709+12 0608 +07 0107 -063607-18350833 340842 350855 JAN 3612 3613+18 3611+13 3609 +07 0105-089900-19990034 990043 230854 UT 0310 3608 +16 3206 +11 2808+06 2517-082518-19 252034 252243 262454 LOU 0105 9900+15 2908+10 2913+05 2825-082731-20 263834 264143 254454 MEM 0109 0108+17 3408+12 3110 +06 2916-072717-19 261934 262144 262555 MKC 0316 0211+11 3409+07 3013+03 2728-10 2638-21 265036 265645 276356 MSY 0315 0216 +19 0315+13 0414+07 0510-080805-20990034 990043 210854 OKC 0715 0810+14 1106+10 9900+05 2414-082419-19 252534 252743 272754 SAT 1107 1713+18 1813+13 1911+07 2006 -071906-19 180734 170743 990054 SOF 0414 0410+14 3605+09 2908+04 2624-092832-20 254135 264444 264655- SHV 0509 9900+18 9900+12 2106 +06 2012-082109-19 220734 240743 260754 STL 0314 0110 +12 3210+08 2915+03 2730-092741-21 265435 265744 288055 TUS 0807+23 0814+16 0814+10 0810-050505-17330533 310842 290954

FIGURE 125.Winds and Temperatures Aloft Forecast.

312

110 SHADED AREAS.... IFR WITH CIS LESS THAN 1000 FT AND/ON VSNY LESS THAI 3 NI

CONTOURED WITHOUT IHADINS MUIR AREAS WITH CIS SREATER WEATHER DEPICTION THAN OR EQUAL TO 1000 TO LESS THAN OR [QUAL TO woo FT )1. 10Z FRI OS SEP 1988 AND/ON VSSY 'NEATEN THAN OR EQUAL TO 3 TO LESS THAN OR ETL TO 6 MI

NO CONTOURS , A FRONTS VALID 092 PRI OS SEP 1966 -R ARIAS WITH CIS GREATER THAN 3600 PT AND VEST UNEATEN THAN 6 NI

FIGURE 126.Weather Depict Ion Chart.

314 313 I133Z FRI 09 SEP 1988 RADAR DUMP TIME 1144Z START 1154Z WARMS RADARSCNA cas VOV

LEGEND... 'ONO-- EON° AREAS CONTOURS AT INTENSITIES -3-5 TOPS In -SAKS 111X--loos OF FT PREFIX-AACFT RPTD TOP 14/31TAREASLINES--PENNANTS MVI:IT--CELLS--AIWKW/3 WITH SPEED PRECIP TYPE AND CHANGE OF INTENSITY 13 NEW OR 114CRS - 13 OCRO N68 D128

315 FIGURE 127.Radar Summary Chart. 316 VT0000Z FRI UP 011 INS II 001141111 OR OOKATIltTOSIOULIDICI) SIII WX PROS .41NR 1.0W LW. SPC 400215 NOD 0111 550

V TOODOZ MI SEP 011 IMO IZMIR SPC PROS VTIE002 FRI SEP 05 15141 NU 1111 550 24NR PC PRO NU D211 550

FIGURE 128.Significant Weather Prognostic Chart

318 317 11556 18+04 %

II \583 20 +05

577 +06 -10 -10 577 %. ...) /-01 -09 81 1 58 + 0NINIZ.Itt/D7 -.06 79 -II 9 .581.414"8-01 +011i +00 11 09 581 587 585 4 +03 11410587 12 +03 -06 586 4 o +03 +gm 58 +04

-02 589 +02

590/81.590 y+03 20 +03 -06' 5861 16 +03 3 +01 -05 591 9 10 14' +0I 113 03 500 C 591 4 591 -901a; .45s al 0 N MO 05\589% i 16%$1/ ./ N014 500M8 ANALYSIS HEIGHTS/TEMPERATURE 00Z AUG 22

FIGURE 129.-500 MB Analysis Heights/Temperature Chart. 114 319 Appendix 3

or! rU 111W IMMI

966 967 _ 916 x 7oz

02969 9 =IV 7.1441%.,.....:

IMO

976 10K 41;3 29 975 111:975 01 .4eoa 15 LV 11 +00 ,10K jel=1(974 -11742 29.. 4 X +pi ..80r mute 31117614,3/4X , 973 15 i/ e le 4.00 10 K. -31 x +10 10 +00 .."" 3972 31 973 X 10K r.10K

30 " -131c.roeNI 11111k? 61°I\s 300MB ANALYSIS HEIGTS/ISOTACHS I2Z MON AUG 88

FIGURE 130.-300 MB Analysis Heights/lsotacha Chart.

, 115 320 18E

WM. isyg... 00K, 4 4 =IND 1 e 7 15 -5T 205 e / t I ,t -041 / 1 K MIMI 11000 ., e 1 )01( 4 /\ % o+/ /4 Ito+1110e'e. . ...1" 10K) -eollip 10 +05 13 sold f es. 0 ON. de 50 1+04 4 117 tl 0 Pa" \ -51 2 --51 7-05t.t0Zr- 11-I% Thal\ 209 +02 +05 4.251 ".41 1.ou r. =h. .411P1' 130 12 OK +00' 11 -53 232 111111111111 Mobs -.-1i ,9...,tiimidoyk. 1 4.07 50K- ...17.r"?, NM 7 It_'_11==1 40 IMIEll xj142:35 9 V TO 4,54:211 +00 ,/ 50K-- '6 TO -51241 01 / /-5 232 -52 42 toter2 4 1 244-.50K- 2_246 +2 -0s 30K 244 OK 251 243 +00/----- 570 -01 AOK- 3/0°. I 10* 252 -52243 OA/ -45 FroSeto% Ida.zil +00 -02 , , 7i5'247164; /035 /50K /v/--01-, -4 1-33T0 e / 10e- -52 .d249 , , -in24r( "51°251 w+00 \-011r-1-631 ,.-5h2,12 -ea oaSa -01 ..., .... 1 ...--1 ---"--,fe''' 702 -01

Who -,3

00-:,1011 ..4 -10K .-10K / -54 2 too +ot

200MB ANALYSISHEIGHTS/ISOTAeHSI2Z MON2iAUG 88

FIGURE 131.-200 MB Analysis Heights/lsotachs Chart.

116 321 FIGURE 132A.Tropopause Pressure.

323 322 GOMA ISHR FCST TROP. STREANS/ISOTACHS VALID ISZ MON U AUG SS

FIGURE 132B.Tropopause/Strearris Isotachs. 325 VT 1522Z AU. HMOS HI LVL $15 WX 400 -TOMS PROS N545 516

FIGURE 132C.High-Level Significant Weather Chart. 327 326 N054A ISHR FCST

FIGURE 132D.TropopausePressure/VHS. BOUNDARY OF THUNDERSTORM AREA SEVERE WEATHER (STORMS EXPECTED TO RIGHT OF LINE) -Ilk OUTLOOK AREA

FIGURE 133A.- -Severe Weather Out! ook (AC). 330 33166 r I V--

NOTE: GENERAL THUNDERSTORM SEVERE WEATHER It'irFORECAST IS NOV INCLUDED Bo OUTLOOK AREA :11.1::;.: t

ITP/oik

1111

SEVERE WEAT ER OUTLOOK (AC) VALID 12Z _i_____TO 12Z Agirr. FCSTRI -ler%

FIGURE 13313.Severe Weather Outlook (AC). Appendix 3

STARS, JULY-DEC., 1978 INTERPOLATION OF G.H.A. erne Deo. Increment to be added for Intervale of G.M.T. to .. G.H.A. of: Sun, Arles (r) and planets; Moon Amur 3.1315 388.40 23 SUN. me. MOON SUN. Na. MOON SUN. Ne. MOON 5 Ackerner 0.6385 46 8. 57 21 M S. ,f6a MI a m aM 4 412 Atria 1.1173 39.8. 62 3900 00 00 00 03 17 03 25 05 52 000 0 50 06 37I 40 19Adam t 1.6255 338. 28 57 01 OC 02 21 03 211 41 06 54 0 01 0 51 1 41 10*Aldebaran t 1.1291 19N. 16 28 05 00 06 25 03 33 45 0 02 0 52 1 4207 00 32Alioth 1.7 09 00 10 29 03 37 49 07 04 166 44N. 56 05 003 0 53 1 43 34Alkaid 1.9153 20N. 49 23 13 00 14 33 03 41 53 07 08 004 0 54 1 44 UAl Na'ir 2.2 28 16 8. 47 04 17 00 18 37 03 4506 57 07 13 0 05 0 55 1 45 15Alnilam t 1.8276 13 8.1 13 21 00 22 41 OS 4907 01 006 0 56 I 4607 17 25Alpkard t 2.2218 228. 834 25 00 26 45 03 54 05 07 21 0 07 0 57 1 47 41'AlpItecat 2.3 126 33N. 26 47 29 00 31 49 03 U G. 07 25 t 0 058 1 48 Alpherats t 2.2358 10N. 28 58 33 00 35 53 04 02 13 07 29 0 09 0 59 1 49 51*Altair t 0.9 82 34N. 8 49 37 00 39 03 57 04 06 17 2 0 10 1 00 1 50 87 28 A nkaa 2.4353 41 8.42 23 41 00 43 04 01 04 10 21 07 37 42'Antares 1.2112 59 0 11 1 01 1 51 t 8.21323 45 00 47 05 04 14 U 07 42 0 12 1 1 52 370Archon, t 0.2146 20N. 19 18 49 00 St 09 04 19 0 13 1 201530748 48Atria 1.9108 248.08 39 53 00 55 13 04 23 07 1141 0 14 104 U 22Avior 1.7234 298.59 2600 57 01 00 1 0 15 17 04 27 87 07 14 111 Dellagrix 1.7 I 55 279 00N. 62001 01 01 04 21 04 31 41 U 16Bete/gem t 5 1- 27180 0 18 1 06 I 58 N. 724 050 01 08 u 04 U 03 08 02 17 1 157 17'Canopus -0.9264088.52 41 09 01 12 29 114 08 06 0 18 1 01 58 12'Capella 0.2281 13N. 45 58 13 01 16 331 08143 53 0 19 1 590811 $3'Dot& 1.8 49 49N. 45 13 17 01 20 37 04 4807 U 08 15 211*Denebola 2.2183 01 0 20 I 10 2 00 N. 14 42 21 01 24 41 04 5208 01 08 19 4*Diphda 1 2.2349 22 8. 18 06 0 21 1 II 2 01 25 01 29 45 04 56 OS 08 U 0 22 1 12 2 27'Dublie 2.0194 24N. 61 52 29 01 33 49 OS 00 0 OS 27 14 1.8 0 23 1 13 2 03 BMA 278 46N. 28 35 480 24 01 37 53 OS 04 13 115 31 47/Dania 2.4 1 14 2 90 58N. 51 30 37 01 4104 57 U 08 171 08 35 54*Bail 2.5 34 13 0 25 I 15 05 N. 9 47 41 01 45 06 01 05 12 21 011 40 romalkaut 1.8 15 538.29 44 0 26 ! 16 2 U 01 49 05 0517 U 08 44 027 1 17 2 111 Oticrus 1.6172 308. 57 00 49 01 53 09 OS 21 29 08 48 29* 0 1 18 2 Gienals 2.8176 208. 17 25 532801 58 13 05 25 33 08 52 35Hadar 0.9 0 29 1 19 209 149 258.60 1601 57 02 02 17 05 2I 87 08 54 IPHamel 1 2.2828 30N. 23 22 0 30 02 01 02 06 2112105 33 411 Kau Ault. 2.084 198.34 24 0 31 1 2 452II911 00 05 02 10 25 05 37 09 04 0 32 2 12 410*Koekab 2.2137 20N. 74 15 09 02 14 191 2205 41 arkab 2.6 0 33 1 23 021800 481N. 15 06 13 02 18 SS 05 46 0 13 toMahar t 2.8314 42 0 34 1 24 2 14 N. 400 17 02 23 37 OS 5008 57 09 17 UMenke* 2.8148 89 8.36 16 0 35 2 15 21 02 27 411 48055409 01 09 21 24'Misplacidue 1.8221 458. 69 38 0 36 1 26 2 18 25 02 31 45 05 58 05 0 25 Mirfak 0 37 1 27 217 1.9309 18N. 49 47 29 02 SS 49 06 02 09 29 Nunki 2.1 76 31 2 18 8. 26 19 330 38 02 U 531 2804 OS IS 09 83 $3'Peacock 2.1 54 008. 56 48 n 19 370390243UN 04 10 09 U 21Pollux 1.2244 00N. 28 05 0 40 1 30 17212 20 41 02 4706 01 N 15 21 Procyon 0.5245 27N. 5 17 0 41 1 31 2 21090 45 02 51 OS 08 19 U 09 46 46Resathague 0 42 I 82 2 22 t 26 31N. 12 35 49 02 56 09 08 23 29 09 50 URegulus 1.3 0 43 1 33 208 12N. 12 04 53 03 00 13 14 37 332 23 01 54 11Rigel 0.3281 37 S. 8 14 0 44 1 84 2 24 02 57 03 04 17 06 31 37 00 Rigil Kent 0.1140 288. 60 45 0 45 1 35 03 01 03 03 225 44&bib 2.6102 438. 15 42 21 06 35 41 100U0 050460312 251380639 452 6 3&kedar 0 47 1 37 2 27 2.5350 10N. 56 25 00 03 16 29 06 44 49 45Shaul. 1.7 0 48 1 38 96 388. 37 05 13 OS 20 33 06 48 0228 18Sirius t-1.6258 578.16 41 0 49 I 39 17 03 25 37 06 5209 572 28 83Spies 1.2158 598. 11 03 0 30 1 40 03 21 os n06 41 06 56 2 30 28WW1 2.2223 12El. 43 21 10 00 4 Vqa 0.1 80 57N. 38 40 *Stars used In 11.0. 249 (A.P. 3270) Vol. 1. 39Ituben'ulti 137 358. 15 57 Mars that may be used with Vols. 2 and 3.

FIGURE134.-STARS, July - December.

123 334 (DAY 262) GREENWICH P. M. 1978 SEPTEMBER 19 (TUESDAY)

0 SUN ANTS VSNUS-4.2AlP1111-1.5SATURN 1.0 0 11100/4 IL., Mom'giff GMT so OHA Dm GSA 1' GSA Oft GSA D.C. GSA Doc. GSA Dec.

1200 i 312 N 130.017802.2321 44' 519 0;53* 0; 1119 51 181 545 N101 23514; 51 N 91 0; II 116 II 10 4 012 30.6180 32.7324 14 55 37 21 25 150 16 08 152 41 20 6 31.9 30.4183 03.1326 44 58 08 23 55 107209 56 55 30 9 01.9 30.1185 33.5329 14 60 38 26 25 156 06 ii7009 42 51 40 11 31.9 30.1188 03.9331 44 63 08 28 56 157 30 13688931 48 5014 02.0 30.0190 34.1334 14 65 39 31 26 159 55 146609 22 45 6409 15 43 13 0016 32.o N 1 292193 04.7336 45 519 OS68 09 N19 5133 56 N10 23162 20 N 9 166209 OS 42 10 19 02.1 29.6195 35.1339 15 70 39 36 27 164 45 17 in ,09 03 20 21 32.1 29.5198 05.5341 45 73 10 38 57 167 10 19" "n'' ', u" ", v, 30 24 022 29.1200 352344 15 75 40 41 27 169 35 200,r2'' 4026 322 29.2203 06.4346 45 78 10 43 58 172 00 22r,a,'' 50 29 022 29.0205 362349 15 80 41 46 28 174 25 23 49 37 5208 46'' 36-' 14 0031 32.2 N 1 282208 072351 45 519 0983 11 N19 5148 59 NIO 23176 SON 9 25,n, ,,2. 10 34 022 28.7210 37.6354 15 85 41 51 29 179 15 26SO- -v.. oa 20 36 323 28.5213 082356 45 88 12 53 59 181 40 284588 36 34 30 39 02.4 28.1215 38.4359 16 90 42 56 30 184 05 294088 30 32 4,41 32.4 282218 082 1 46 93 12 59 00 196 30 3135OS 25 31 50 44 02.4 282220 39.2 4 16 95 43 61 30 196 55 323008 20 30

15 0046 322 N 1 27.9223 092 6 46 519 1098 13 N19 5164 01 NIO 23191 20 N 934Pm088 2,8, 1049 02.5 27.7225 40.1 9 16 100 43 66 31 193 45 35a., 06vw a. 20 51 32.5 27.5228 10.5 11 46 103 14 69 196 10 37 008 00 25 79 8321 198 35. 10 30 54 02.6 27.4230 40.114 16 105 44 3$ 07 54 24 40 56 32.6 27.2233 11216 46 108 14 74 02 201 00 402007 47 22 SO 59 02.7 27.1235 41.7 19 16 110 45 76 33 203 25 413007 40 21 16 0061 32.7 N 1 262238 12221 47 519 11113 15 N19 5179 03 N10 23205 49 N 9 433582 35 20 1064 02.7 26.7240 42.524 17 115 45 81 33 208 14 444082 30 19 2066 322 26.6243 12226 47 118 16 84 04 210 39 464507 25 17 3069 022 26.4245 43.129 17 120 46 86 34 213 04 475082 18 15 4071 322 26.224$ 13.731 47 123 16 89 04 215 29 495207 15 15 5074 022 26.1250 44.234 17 125 47 91 35 217 54 505407 11 14 17 00 76 32.9 N 1 252253 14.636 47 519 12128 17 N19 Si94 05 NIO 22220 19 N 9 525682 " 13 10 79 03.0 252255 45.039 17 130 47 96 35 222 44 535807 03 12 2081 33.0 252258 15241 47 133 18 99 06 225 09 556086 59 11 3084 03.o 25.4260 45244 18 135 48 101 36 227 34 56s 4086 332 25.1263 16.246 48 138 18 104 06 229 59 58 5089 03.1 25.1265 46249 18 140 49 106 37 232 24 9 59 1 8 0091 33.1 N 1 25.0265 17.o51 48 519 12143 19 NI9 Si109 07 NIO 22234 49 NIO 01kW. P. in k 1094 032 242270 47.454 II 145 49 111 38 237 14 02 r096 332 24.6273 17.956 48 148 20 114 08 239 39 04 Sot 3099 03.2 24.5275 48.159 18 150 50 116 38 242 04 05 ' 40101 332 24.1278 18.761 48 153 20 119 09 244 29 06 + + 50104 032 24.12$0 49.164 18 155 51 121 39 246 54 OS 0 . 55 ' m 57eL32 19 00106 33.4 N 1 242283 19366 49 519 13158 21 N19 51124 09 N10 22249 19 NIO 09-.: 56r. 31 10109 03.4 232285 49269 19 160 51 126 40 251 44 11L.553/ in 20111 33.4 23.7288 20271 49 163 22 129 10 234 09 121$ ,59-,.- 30114 03.5 23.5290 50.774 19 165 52 131 41 256 34 1421 ;-;60 L' 40116 33.5 23.1293 21.176 49 168 22 134 11 258 59 1523 61 - 50119 03.5 23.229! 51479 19 170 53 136 41 261 24 1726 5262 27 .16SiLe26 20 00121 33.6 N 1 23.0298 22.081 49 519 14173 23 N19 50139 12 NIO 22263 48 N10 186.anwho 25 10124 03.6 222300 52.454 19 175 53 141 42 266 13 1930 --64 20126 33.7 22.7303 22286 50 178 24 144 12 268 38 21n496 5 24 30129 03.7 22.5305 53.2 89 20 180 54 146 43 271 03 2234 4$66 23 40131 33.7 22.4308 23.6 91 50 183 25 149 13 273 28 2435 4766 22 50134 032 22.2310 54.094 20 105 55 151 43 275 S3 25 46 21 37 69 2100136 332 N 1 22.0313 24.4 96 50 519 1518$ 25 N19 50154 14 NIO 22278 18 NIO 2739 4570 20 10139 032 212315 54299 20 190 56 156 44 280 43 2840 4473 19 20141 332 21.7318 25.2101 50 193 26 159 14 283 08 2942 4372 18 30144 03.9 21.6320 55.7104 20 195 56 161 45 285 33 31 42 17 40146 34.0 21.4323 26.1106 50 198 27 164 15 287 58 3243417316 SO149 042 21.2325 56.5109 21 200 57 166 46 290 23 3445 4074 15 46 75 12 00151 34.o N 1 21.1328 262111 Si 519 16203 27 N19 50169 16 NIO 22292 48 N10 3547 3474 14 10154 04.1 202330 Si.)114 21 205 511 171 46 295 13 3749 3822 13 20156 342 20.7333 27.7116 SI 208 28 174 17 297 38 38ch 37,ik 12 30159 04.1 20.6335 58.1119 21 210 58 176 47 300 03 39r. 36...'- ii 40161 34.2 20.4338 28.5121 Si 213 29 179 17 302 28 41.4 35IT10 50164 04.2 202340 38.4124 21 215 59 181 48 304 53 4253 00 0 00166 34.2 N 1 20.1343 29.4126 51 519 17218 29 $19 50114 18 NIO 22307 18 N10 44 33 10169 04.1 192345 592129 21 221 00 186 48 309 43 45,aSS 32 10171 343 19.4348 30.2131 52 223 30 189 19 312 OS 4626 30174 04.4 192351 00.6134 22 226 00 191 49 314 33 48Sun SO 15!9 40176 34.4 19.5353 31.0136 52 228 31 194 20 316 58 49 SO179 04.4 19.1356 01.4139 22 231 01 196 SO 319 23 SiMoon SO 16' Ono 15 612 SO 01.0 15 00 7 SO 00.9 15 02.0 SO 00.1 15 02.2 SO 00.1 14 KCVO OSA Age 174

FIGURE 135.-Greenwich Day 262.

124 335 Appendix 3

(DAY 263) GREENWICH A. M. 1978 SEPTEMBER 20 (WEDNESDAY)

GMT 0 SUN A11111 V1NUS-4.2JUN TIN-1.1SAIUIN 1.0 0 MOON 014A Du. ONA T ONA Dec ONA 04N. ONA DK. ONA DN. 110 I I 4.0 III I IN 358 31.5 I 181 34.3 N 1 19.1 I I 141 52 519 11 00 00 233 31 N19 50199 20 N10 22321 48 N10 52 0 10184 04.3 19.o 1 02.2140 22 236 02 201 Si 324 13 53 I 0 20116 34.5 11.0 3 324106 52 238 32 204 21 326 31 55721807-02 30119 040 11.0 6 03.1149 22 241 02 206 51 329 03 567018 31+03 40191 14.5 18.3 8 33.5151 52 243 33 209 22 3312$ s6818 49 06 50194 04.7 11.3 11 03.3150 23 206 03 211 52 333 53 10 596619 84 89 6419 17 11 01 001% 34.7 N 1 18.2 13 34.3156 53 519 18241 33 N19 50214 22 N10 22336 18 N11 006219 27 12 10199 04.7 18.0 16 04.7151 23 251 04 216 53 33142 026019 36 13 20201 34.0 17.0 18 35.a161 53 253 34 219 23 341 07 03 343 32 . 19 44 14 30204 04.5 17.7 2105.5160 23 256 04 221 50 05 40206 34J 17.5 23 35.0166 53 25135 224 24 345 57 06865619 51 15 50209 04A 17.426 WI169 23 261 05 226 50 348 22 075619 57 16 5220 03 17 02 00211 34.5 N 1 17.228 36.7171 53 519 19263 35 119 50229 25 N10 21350 47 N1101 10214 05.0 17.03107.2174 24 266 06 231 55 353 12 105820 88 17 20216 35.0 16A33 37.6176 54 261 36 234 25 355 37 ii4520 19 19 30219 05.0 16.7 36 08.0179 24 271 06 236 56 3% 02 134828 28 20 40221 35.a 16.5 3$ 31.0181 54 273 37 239 26 0 27 143528-36 21 50224 05.1 16.4410$.0180 24 276 07 241 56 2 52 163020 43 21 03 00226 35.1 N 1 16.2 43 39.2186.54 519 20278 37 N19 50244 27 N10 21 5 17 N11 172028 55 23 10221 051 16.1 46 094189 24 281 08 246 57 7 42 111021 06 24 20231 351 15304 40.o191 54 M 38 249 28 10 07 20 021 1625 30234 05.3 15.7 51 10J194 24 286 08 251 58 12 32 .211021 26 26 20 40236 35.3 15.0 53 40.5196 55 288 39 254 28 14 57 22 21 37 27 SO23905.3 BA56 113199 25 291 09 256 59 17 22 243021 49 29 04 00241 35.4 N 1 15.358 01.7201 55 519 21293 39 119 SO259 29 110 2119 47 N11 253521 56 29 10124005.0 15.1 61 12.1204 25 296 10 30 261 59 2422 3712 264022 85 20246 35.4 14.0 63 42.5206 55 298 40 264 30 2$4522 14 31 50 30249 05.5 14.0 66 12.0209 25 301 10 267 1^ 27 02 21 22 26 33 40251 35.3 10.6 68 03.3211 55 303 41 269 .,,, 29 27 305222 31 33 SO254 053 14.4 71 13.7214 25 306 11 272 01 31 52 325422 37 34 OS 00256 354 N 1 14.3 73 44.1216 56 519 22308 41 N19 SO274 31 110 2134 17 111 335622 44 34 10259 054 14.1 76 10.5 219 26 311 12 277 01 36 02 342"22 nn52 2 20261 35.7 14.o 7145.0221 56 313 42 279 32 39 07 36 - -- 30264 05.7 13.4 81 15.4224 26 316 12 282 02 41 32 37s 40266 35.7 13.0 53 45.0226 56 31$ 43 284 33 43 57 38 SO26105.0 13.5 36 16.2229 26 321 13 287 03 44 22 40 06 00271 35.0 N 1 13.3 88 46.613156 519 23323 43 119 50289 33 N10 21NI 47 N11411681 P. in A' 10274 054 13.1 91 17.0234 26 326 14 292 04 51 12 42 20276 35A 13.093 07.0236 56 328 44 214 34 53 37 441 AIS 3027905.0 12.096 17.8239 27 331 14 297 04 56 02 45 4028136.0 12.7 9141.2201 57 333 45 299 35 58 27 46 + + SO144 06.o 12.3101 18.7244 27 336 15 302 OS 60 52 41 0' SS ' rA32 07 00216 364 N 1 12.3103 09.1246 57 519 2433145 119 49304 36 110 2163 17 N1149I ,.., 31 10289 06.1 12.2106 19.5249 27 341 16 307 06 65 02 50aa ar 30 2029136.1 12.010149.0251 57 343 46 309 36 48 07 5217 50 302% 06.1 114III 20.3254 27 346 16 312 07 70 32 5320 40 40296 361 11.7113 50.7256 57 34147 314 37 72 57 5423 61 88 50299 064 11.3116 21.1239 27 351 17 317 07 75 22 SS23 6227 L.26 00 00301 %a N 1 11.411151.5261 58 519 24353 47 N19 49319 38 110 2177 47 111 5727 2 501. 10100 06.3 11.2121 21A264 28 356 18 322 08 80 12 5828 6425 20306 36.3 114123 524260 58 35148 324 38 82 37 11 5131 4965 24 30309 064 10.3126 22.0269 28 1 18 327 09 85 02 12 01334866 2) 40311 36.4 10.7 128 53.2271 58 3 49 329 39 07 27 02VI476722 50314 064 10.413123.0270 28 6 19 332 09 89 52 03if 466 21 09 316 36.3 N 1 10.4133 54.0276 58 519 25 8 41 N19 41334 40 110 2192 17 112 05 4570 20,, 1031906.5 10.2136 240279 28 11 20 337 10 90 42 0640 -71 - 20321 36.5 10.1138 54.8281 59 13 50 339 41 97 07 07j41 1372 10 30324 064 09.0101 25.22114 29 16 20 342 11 99 32 08 42 17 40326 364 09.0143 554286 59 10 51 344 41 1043 73 SO 329 06.7 094146 264289 29 21 21 34712 1104012527 '-'m 464401 7524 1136 10 00331 36.7 N 109.4148 56.5291 59 519 2623 51 N19 49349 42 110 21106 47 N12 1247 3976 14 10334 06.7 09.3151 26.0294 29 26 22 352 12 109 12 14 37713 20336 364 09.1153 57.3296 59 2152 354 43 111 37 1550 377012 30339 064 08.9156 27.7299 21 31 22 357 13 114 02 16n.26...11 40341 36J 01.015158.1301 51 33 53 359 43 116 27 17!!52 10 50344 06.5 08.0141 28.5304 30 36 23 2 14 118 52 19 OU 932$34 11 00144 36.0 N 10$.5263 511.5302 00 519 27NI 54 119 49 444 110 20121 17 N12 20-R.33 10349 07.0 01.3166 29.3309 30 41 24 7 15 123 41 21SS32 20351 37.0 01.1168 59.7312 00 43 54 9 05 126 06 2258 08.0 354 07.0 17130.2314 30 0625 12 1S 128 31 24sunSD7, ls:0 .....140356 37.1 07.0174 004317 00 0855 14 46 130 56 25 SO3% 07.1 07.4176 31.0319 30 51 25 17 16 133 21 26 SD 16' loss 15 NJ So 01.0 1500.7 S000. 15 02.0 5000.1 1503.2 SO 00.1 N NJ *) NJ AIN UN

FIGURE 136. - Greenwich Day 283.

336 125 (DAY 263) GREENWICH P. M. 1978 SEPTEMBER 20 (WEDNESDAY)

GMT 0 SUN AMU VINUS-4.2JUNTIR-1.5SATURN 1.0 0 MOON Lo,4,0en- 004 0t14 Dec. DMA 'Y' DMA D.c. GM Doc DNA Dec 084 D.c. 4t

12 Oil 2 37.1 N 2 07.5179 01.4322 00 S19 2653 56 $1; 4;19 46 $10 2013; 46 $12 27 N 10 4 07.2 07.3181 319324 31 56 26 22 17 138 11 29 to at a 20 6 37.2 07.2184 02.2327 01 58 56 24 47 140 36 307211 45 54 30 1 07.5 07.0186 32.6329 31 61 27 27 17. . 147 01 . 317011 22 49 40 11 37.3 06.4189 03.o332 01 63 57 29 48 145 26 326811 04 45 50 14 07.3 06.7191 33.4334 31 66 27 32 1$ 147 51 346610 50 43 6410 39 41 13 0016 37.4 N 1 061194 039337 01 S19 2968 S8 N19 4934 49 N10 20150 16 N12 356210 29 39 10 19 07.4 06.4196 34.3339 31 71 28 37 19 152 41 36 20 21 37.4 06.2199 04.7342 01 73 58 39 49 195 06 376010 21 38 3024 07.s 06.0201 35.1344 31 76 29 42 20 157 31 39Se18 13 37 40 26 37.s 05.9204 OS.s347 02 78 59 44 50 159 56 40 _56 ,12 .0,7 3.6. 50 29 07.5 05.7206 35.9349 32 81 29 47 20 162 21 41 ." A VA 522009 S6 34" 14 003: 37.6 N 1 OS.s209 06.33S2 02 S19 2984 00 619 4949 S1 $10 20164 46 N12 42 10 34 07.6 05.4211 36.7354 32 86 30 52 21 167 11 4430041 51 33 2036 37.7 05.2214 07.1357 02 89 00 54 51 169 36 454509 41 32 3039 07.7 05.1216 37.s359 32 91 31 57 22 172 01 464089 33 31 4041 37.7 049219 08.0 2 02 94 01 S9 S2 174 26 473509 26 30 30 50 44 079 04.7221 38.4 4 32 96 31 62 23 176 51 48 09 19 29 15 0046 379 N 1 04.6224 08.5 7 03 S19 3099 02 N19 4964 53 610 20179 16 N12 502889 89 28 10 49 079 04.4226 39.2 9 33 101 32 67 23 In 41 511008 59 26 20 51 379 043229 09412 03 104 02 69 S4 184 06 52 0OS 50 25 10 30 S4 072 04.1231 40.o14 33 106 33 72 24 186 31 53 88 41 24 4056 38.0 03.4234 10.4 17 03 109 03 74 54 144 56 542008 32 23 50 59 08.0 039236 409 19 33 111 33 77 25 191 21 S63008 21 21 20 16 0061 38.0$ 1 03.6239 11.222 03 S19 31114 04 $19 4979 S5 $10 20193 46 $12 S735(11/ 15 10 64 08.1 03.4241 41.724 33 116 34 82 25 196 11 SI4088 88 19 2066 38.1 03.5244 12.127 04 119 04 84 56 198 36 12 594587 59 18 3069 08.1 03.1246 42.s29 34 121 35 87 26 201 0113 015007 49 17 40 71 38.2 03.0 249 12.032 04 124 OS 89 57 203 26 023207 43 16 50 74 05.2 029251 43.334 34 126 35 92 27 205 51 035407 40 15 17 0076 383 N 1 024254 13.737 04 S19 32129 06 N19 4894 57 N10 20208 16 N13 045687 34 14 10 71 08.3 02.s236 44.139 34 131 36 97 28 210 41 05SS07 28 14 60 2081 38.5 02.3259 14.542 04 134 06 99 58 213 06 06 07 21 12 3084 08.4 02.1261 44.944 34 136 37 102 28 215 31 08 4086 38.4 02.o264 15.547 04 139 07 104 59 217 S6 09S SO 89 08.4 014266 45.s49 35 141 37 107 29 220 21 10 110091 38.5 N 1 01.7269 16.2 52 05 S19 33144 08 619 48109 59 N10 20222 46 N13 11 616".6° '^ A' 10 94 08.3 01.5271 46.0S4 35 146 38 112 30 225 11 12 2096 38.5 01.3274 17.057 05 149 08 115 00 227 36 14 is. i 30 99 082 01.2276 47.459 35 151 39 117 31 230 01 15 u u 40101 38.6 01.0279 179 62 OS 154 09 120 01 232 26 16 + + SO104 08.7 009281 48.264 35 156 39 122 31 234 51 17 54 20 S' 32 19 00106 38.7 N 1 00.7284 18967 05 S19 34159 10 619 48125 02 N10 20237 16 N13 18.; 56:: 31 10109 08.7 00.5286 49.069 36 161 40 127 32 239 41 19 21 ll" 30 2011135.5 00.4289 19.572 06 164 10 130 02 242 06 2115 -- 54St 29" 30114 089 00.2291 49.974 36 166 41 132 33 244 31 2219 .259 40116 38.8 1 009294 20377 06 169 11 135 03 246 56 23n --6028 50119 089 0 59.92% 50.779 36 171 41 137 33 249 21 2424 5262 27 20 00121 382 6 0 59.7299 21.182 06 S19 34174 12 619 48140 04 610 19251 46 61: 2526 3163 26 50 10124 09.0 592301 51.584 36 176 42 142 34 254 11 2629 6425 24 20126 39.0 59.4304 21.987 06 179 12 145 05 256 36 2731 4965 30129 09.0 59.2306 52.389 36 181 43 147 35 259 01 2932 4866 23 40131 39.1 59.1309 22.792 07 184 13 150 05 261 26 3094 470 22 50134 09.1 582311 S3.294 37 186 43 152 36 263 32 31ii 46u 21 21 00136 39.1 $ 0 58.7314 23.697 07 S19 35189 14 619 481SS 06 N10 19266 17 613 3235 4569 20 10139 09.2 584316 54.099 37 191 44 157 36 268 42 3339 4470 19 20141 39.2 58.4319 24.4102 07 194 14 160 07 271 07 3441 4371 18 30144 09.2 58.3321 34.4104 37 196 45 162 37 273 32 35 42 17 40146 39a 58.1324 25.2107 07 199 15 165 07 275 57 3742A, 41..,73 16 50149 093 57.9326 55.6109 37 201 45 167 38 275 22 38"" 40/9 13 45 75 22 00151 39.4 N 0 57.0329 26.o112 08 S19 36204 16 $19 48170 08 $10 19280 47 $13 3947 3976 14 10154 09.4 574331 S6.4114 38 206 46 172 38 283 12 4046 3877 13 20156 39.4 57.5334 26.5117 08 209 16 175 09 285 37 41A, 37 12 30159 09.1 57.3336 57.3119 38 211 47 177 39 288 02 42 3671 11 40161 39.5 57.1339 27.7122 08 214 17 180 10 290 27 43 21357910 SO164 09.s 57.0341 58.1124 38 216 47 182 40 292 52 44S2 34 110 23 00166 39.6 N 0 564344 28.5127 08 S19 37219 13 $19 48185 10 610 19295 17 $13 46an 33 10169 09.6 564346 582129 38 221 48 187 41 297 42 47 32 20171 39.7 56.s349 29.3132 09 224 18 190 11 300 07 4820 30174 09.7 56.3351 59.7134 39 226 49 192 41 302 32 49Sun SD 16:0 40176 39.7 56.2354 30.1137 09 229 19 195 12 304 57 50 50179 094 56.0357 00.5139 39 231 49 197 42 307 22 51Moon SD 15' W. 15 002 SO 01.0 15 00.7 50 00.5 15 02.0 SO 00.1 15 02.2 SO 00.1 14 30.0 NO 07.1 Ago 18d

FIGURE 137.- Greenwich Day 283.

126337 Appendix 3

POLARIS (POLE STAR) TABLE, 1978 FOR DETERMINING THE LATITUDE FROM A SEXTANT ALTITUDE

L. H. A. et, L. H.A. T' L.H. A. I' L. H.A. T' L. H. A. I' L. H.A. I' L. H. A. I' L. H. A. I' Q Q Q Q Q I I , I I Q Q < . I I , I 159N 81 54 114 52 145 20 188 06 X8 21 310 18 - 42 -32 - 6 +20 +46 +28 331 10 1 12 83 u 116 01 146 35 191 03 249 44 301 27+ 2 -24 43 -31 - 5 +21 +47 +27 + 1 332 23 3 X 84 50 117 10 147 51 194 26 271 06 302 311 333 47-2: -44 -30 4 +22 +48 0 5 50 86 16 118 19 149 08 198 34 272 27+26383 45 US 07-2( - 45 - 29 - 3 +23 +49 +25 1 8 27 87 40 119 28 150 26 X14 34 373 46 364 54- -21 -as -28 - 2 +24 +50 +24 U6 U 11 21 N 02 1211 37 151 45 o55 05 306 03- 2 -21 47 -27 - 1 +25n +49M +23 337 51, 14 42 SO 24 121 46 153 04 224 55 276 23 307 12 3 -24 - -26 0 +26 +48 +22 4 U9 15 18 48 91 44 i nU 154 25 231 05 277 40 308 21 -3( 49 -25 + 1 +27 +47 +21 340 41 24 411 93 03 124 04 155 47 234 28 278 56 309 30- 5 -31 -50 -24 + 2 +28 +46 +20 6342 08 40 48 94 21 125 13 157 10 337 25 388 11 3111 U- -3: 49 -23 + 3 +29 +45 +19 343 37 46 48 95 38 126 22 168 35 240 04 281 25 311 48 7 3( 48 -22 + 4 +30 +44 +18 345 08 N42 96 54 127 31 160 01 242 30 282 32 312 58- 8 -34 -47 -21 + 5 +31 +43 +17 246 42 54 10 98 10 128 40 161 29 244 46 283 53 314 08- 9348 18-3: -46 -20 + 6 +32 +42 +15 -10 -31 57 X 9925 129 49 162 59 244 53 285 OS 315 18 349 56 -45 -19 + 7 +33 +15 11 59 41 IN U 130 59 164 31 284 18 316 28 31 -44 -18 + 8 +34248 N+40 +14 351 38 62 15 1111 52 132 119 166 N 350 49 287 29 317 30-12 -3/ -43 -17 + 9 +35 +39 +13 -13353 23-3( 64 19 103 05 133 19 167 42 252 40 288 41 318 50 355 12 is -42154 Is 15 ,,, +10 +38,,, ,,, +38 +12 -14 ,,, 4( -41 -15 ".. '' +11 ''' +37'''' ... +37 68 X 105 SO 135 39 171 115 256 N 2111'''' 02 +11 321 13 -40 -14 +12 +38 +10 -1813359. 01-4(41 70 19 106 41 136 50 172 51 257 49 2112 12 au 26 1 12 -39 -13 +13 +39 +35 + 9 -17 -4:; 72 MI 107 52 138 02 174 42 259 25 203 22 326 -n -12 +14 +40 +34 + au a,-18 -44 73 53 10903 139 13 176 37 261 00 294 33 324 53 5 50 -37 11 +15 +41 +33 + 7 19 75 36 .110 13 140 26 178 38 202 32 295 42 326 06 4; - 10 +16 +42 +32 8 27 77 13 111 23 141 U _,_,, 180 45 + -20 -4( 9 264 02 296 51 327 21 11 21 A. 78 49-5112 33 142 52 -'-`' 183 01 -1.'",,,, 16.+31 + 5, ,,, -21 -X - 8 +18 +44 +30 14 42-41 -'' SO 23 113 43 144 66 185 27 2$6''' 56 ; + 4329'''' -' 53 -22 18 43 -33 - 7 +19 +45 +29 + 3 -23 -44 81 54 114 52 145 211 188 01 208 21 300 18 331 10 i 24 43 Q, which does not include refraction, is to be applied to the corrected 'sextant altitud3 of Polaris. Polaris: Mag. 2.1, S. H. A. 327'14', Dec. N. 89'10.'0

AZIMUTH OF POLARIS

Latitude L.H.A. L.H.A. Latitude fr er 0'30' 50' 55'60' 65'70' 0'30' 50' 55° W 65'70' . . . . 0 0.5 0 0.7 0 8 0.9 1.1 1.4 180 359.5359.5359.3359.2359.1 359.0358 7 10 0.30.4 0.3 0.6 0 7 0 8 1.0 190 359.7359.6359.5359 4359.4359.3359.1 20 0.20 2 0 3 0.3 0.4 0.40 6 200 359.8359.8359 7359.7359.8359.6359.5 30 0.00.0 0.1 0.1 0 1 0.1 0 1 210 0.00.0359.9359.9359.9359.9339.9 40 359.9359 9339.8359 8359 8359 7339 7 220 0.1 0 1 0.2 0 2 0.2 0 20.3

50 359.8359.7 359.6359.6359.5 339.4339.3 230 0.20.3 0.4 0.4 0.3 060.7 66 359.63596359.4359.3359.2359.1358.8 240 0.40 4 0.6 0.7 0.7 0.9 1.1 70 359.5359.4359.2359.1359.0358 8358.5 250 0.50 6 0.8 0.9 1.0 1.2 1.4 SO 359.4359 3359.0358.9358.8338.5358 2 260 0607 0.9 1.1 1.2 1.4 1.7 96 359.3359.2358.9358.8358 6358 3337.9 270 0.70.8 1.1 1.2 14 1.6 2.0

IN 359.2359.1 358.8338.6358.4358.2357.7 0.80.9 1.2 1.3 1.5 1.8 2.2 110 359.2359.1 358.7358.6358.4358.1357.6 290 0.80.9 1.3 14 1.6 1.92.4 359.2359.0338.7358.5358.3358.0357.6 300 0.8 1.0 1.3 1.4 17 2.02.4 130 339.2359.0358.7358.6358.4 358.1357.6 310 0.8 1.0 1.3 1.4 1.7 2.02.4 140 359.2359.1 358.8358.0358.4 3.38.1357.7 320 0.80.9 12 1.4 1.6 1.92.4

150 359.3359.1 358.9358.7358.5358.3357.9 330 0.70.9 1.2 1.3 1.3 1.82.2 160 359.3359.2359.0358.9358.7 358..5338.1 340 0.70.8 1.0 1.2 1.3 1.62.0 170 359.4359.4 359.1359.0358.9358.7358.4 350 0.60.7 0.9 1.0 12 1.4 1.7 IN 359.5359.5359.3359.2359.1 359.0358.7 340 0.50.5 0.7 0.8 0.9 1.1 1.4

When Cassiopeia is left (right), Polaris is west (east).

FIGURE138.-Polaris (Pole Ster,able.

127 338 CORRECTIONS TO BE APPLIED TO SEXTANT ALTITUDE REFRACTION To be subtracted from sextant altitude (referred to m observed altitude in A.P. 3270) Height above sea level in units of t 000 ft. R=II.xf

to I 1 g 25 2 as 30 35 40 I 45 ss I s R.ao vo II 22 SextantAltitude R ., 000 I ISIS 0,90 90 90 90 90 90 90 90 90 90 90 90 0 o 0 o o 63 59 SS 51 46 41 36 3t a6 20 17 13 2 26 22 19 :6 14 It 9 tit 1 .1.1 09 7 6 4 2 2 2 222 21 19 :6 14 12 :0 8 7 S 4 2401 40 lv A 14 12 tO 8 7 i 6 5 3 10 120 3 4 1 30 040 33 3 4 12 II gl 8 7 5 2 to 1 3o 039 +0054 4 4 4S 3 4003 10 6:0 9 7 550 4S03 So 3 10220I30 0 49 +oils -019S 5S S 6 8 to6 so5 50 4 50 4003 no 220 I SO 1 10 024 -0 11 -0 38 6 305 50s oo 4 cm 3 :co 2 30 7 67 8 8 8 1 SO 1 30 * 3a+ci e4 -0 38 -0 34a 6005 104 10 3 20240200 1 30 1000 19-0 13 _. so 78 9 10 9 -043-t on 5204 303 40 2 so2 tO1 40 I 100 35 +0 03-o 27 -0 53 -t to. 8 9 10 tt ico , 20 4 303 40250 220140 Ito0 37 +0 :: -016- 043- 108 -131 9 Mt II I2 23 23 3302 SO 2 10 1 40 / 10034+009 -o :4 -037 I: 23 13 14 24 -1 o -1 :3 -: +4 2 SO2 IO 140 Ito0 37 +0 to-o 13 -0 34 -co 53-1 14 -: 35 -t 5614 13 2416 15 17 2 20140120 0 43 +015 -008-o 31 -0 52-108-1 :7 -1 46 -3 05 28 150120 049+0 :3 -0 02 -0 :6- 046 - 106 -122- 139 - 157 -21420I.tt .I ao 22 I 12044 +o 19-o 06 -o :8 -o 48-109 -1 27 -: 43-1 $d -2 14 -2 30 IS 20 22 24 a3 2522 as 28 30 o 34 +0 10 -0 13-co 36 -055 -: 14-: 32 -1 st -2 06-2 21 -2 34 -2 49..-- 312.+o o6-o16 -o 37-059 -: 17 -: 33-151-307 -2 23-2 37 -25s -3 044.'7- 2,7,'P.; 3031 3.. 3a 31 a.-0 A -0 37 -0 58-1 :6 -t 34 -1 49-306-a as -2 35-2 49 -3 03 -3 16 ji Am" ' .A" 40 -co 53 -1 14- 131 - 147 -203-2 :8 -2 33 -2 47 46 -2 S9 -3 13 -3 XS..- A30 -rgii "40 '- -i io -1 28- 144-159 -215- 228 - 243 -256- 308 -322-33343le in-."' 5° SS: 40-1 53 -0 09 -2 24-338- 252-304-3 17 -3 29 -3 41":,A.',. . -gc ii; 66 SS 49 -3 03 -2 ill -2 33-2 46 -3 0: -3 13-3 25 -3 37 -3 48 ._--- flo gos+ .. go 72 -2 S3 -307 -3 19-3 31 -342 -3 S3

,.1 0 3 10 as 2s as se 40 1 0.9 vo 1.2 PS J n I a 1. n Temperaturein T. I I +47+36+27 + al 4-10 + 3- 5-13 Where R. is 0'9+36+a)+ 6- 4-13-22 -3:-40 For these heights no 0-9 , ve temperature correction /4less than 14 + 5 5 -15-25-36-46 -57-68 isnecessary,so we or the height 22 , greaterthen -to-35-36-46-58-71 1 -83-95 R = R. 2I 2.2 1.23s out ft. use -37-4S-S0-67 -8v -95 I R = R. Choose the column appropriate to height, in units of : 000 ft., and find the range of altitude in which the sextant altitude lies;the corresponding value of R. is the refraction, to be subtracted from sextant altitude, unless conditions are extreme.In that cam find I from the lower table, with critical argument temperature. Use the table on the right to form the refraction, R = R. x I. CORIOLIS (Z) CORRECTION To be applied by moving the position line a distance Z to starboard (right) of the track in northern latitudes and to port (left) in southern latitudes.

G/S Latitude GAS Latitude KNOTS 1 0* leace 3o.I 40 . 50. 160° 700 180° 90° KNOTS e le2e 3e4o° so°6o° 7e80° 9o' ,,,,IS,,,1,, , , IIII.0II

250 0 1 1 I 2 3 3 34 1 44 550 0 3 S 7 9 11 12 1414 14 2 0 0 S S 600 0358:cots 14 15 t6 16 250 0 1 23 4 S 6 6 67 6so o3 69 11:3 is i6 17 17 300 0 I 34 S 6 77 88 700 03 6 912 14 :6 17ill :8 sso 0 2 35 67 8 99 9 750 03 7 to:3 is17 t819 20 400 02 45 78 9 toto to Soo 04 7 to:3 t6t8 2021 21 490 02 4 6 89 to II 12 12 850 04 8 t 1 i4 17 19 21 22 22 500 02 4 7 8 toIt 12t3 13 600 04 8 1215 1820 2223 24

FIGURE 139.Sextant Apaude Corrections.

128 339 Appendix 3

LAT 32111 LAT 3214 ION MtZ.lk I'm He 2n He Zn He 2n He Zn Me Zn WA Me Zn Mc Zn Me Zn He 2n He 2n He Mg T 2n Zn UN Nam 4/011111. P1CA MOWS 741111 Sabo HMI AAA HWY MAKS 4101111/11 *NW IWO Ili 19 10243 0 N2S715 NS4214 15157 20 2035 17 1141044 347 27056 21 05555 35 126) 016 16617 39 20338 15 27040 )4 004146 144 3150 Oil44 26 012Si 04 10542 32 15356 34 24034 211 214511 32 146 27117 03 0555413 128le 28 1672711 104)7 24 271N 55 III41)3 344 1414 14145 16 1111151 51 11643 15 1S455 51 34133 N 10SI 19 145 Iii57 45 05556 55 1010 19 16826 57 203)6 11 1710 16 11841 19 344 1$ 11 N146 '3 N359 42 1174) )7 15555 07 241)149 10SIN 06 745 38 26 0S457 34 1)0)04+ 0 1026 15 106)5 41 1713117 1184105 05 )44 150 On461A .1414 30 IN41 51 15654 11 24311 40 18557 51 344 59 07 054SI 11 13210 N 17026 11 10714 51 27137 58 11040 51 344 1033 ON0 4111111461 19 11944 17 IN5) )6 24411 11 111657 311 74) 344 17 0 Ni411 )9 NI62 06 111144 )6 15951 SI 245JO 22 21657 2) 142 1768 30 05159 27 1151 14 17225 25 20911 09 27))6 41 11140 22 74 / 17 N ossn n 110562 54 11144 54 16052 04 24621 33 211657 07 142 61 10 OS)111103 1161 12117)25 00 210)2 19 27416 02 HI40 07 141 1131 115511 211 INS61 41 11345 111 16251 17 24728 45 28756 50 741 IN61 51 05160 /7 136/I 26 17424 0 210112/ 27415 24 11119 52 143 19 le 16151 11 ON64 20 11445 26161SI 311 24427 56 20756 0 340 2 62 )1 05261 11 14031 11 17524 09 21110 /7 27574 45 11119 JS 741 NN ON12 02 onss 14 11545 40 16449 42 2492714 20156 16 )19 6621 4) 14111 )5 17624 42 21229 47 27574 07 11139 2/ 74) I 1.44 On52 52 05766 NI 11645 5) 166411 55 25026 19 INSS SS 114 1667 5121 025221 15 14)11 38 17721 14 21/211 56 1760 29 111)9 07 74) 11 17 05753 43 N71445 11846 05 16740 07 25125 11 20155 19 110 14)1 05162 44 1451140 17822 46 21428 OS 27612 51 11131 SI 741 22 III OR54 14 01167 10 11946 16 169471/ 252244) 20SS 20 3/1 M65 10 0500 I) 14711 41 17922 10 21527 15 27712 12 1123617 742 22 12 857SS n soes 14 12146 23 17046 /0 25/23 54 0955 00 07 65 49 0496) 40 14611 41 10121 49 21526 24 27711 15 112n 22 742 11141146 0111 lbsolhouHAT/113 MCA 410811111 kko 701p100 foN ALVA UMW 131111111 MIMI ION 110 1106141 4541 lN: C1: 156 Ort:::: tir:: t1:::5: 2::2r:::4:: 1: t ::::3 :tii 11111111111111111:1111;1111111 11 45 51 0102510II 11511 26 27 01114 37 13546 46 1744414 NS53 59 115 26 41 07147 51 II/64 52 1552010 21821 51 27929 41 11237 /5 742 4410 N6843 05927 11 09215 13 11546 51 1764) 14 2565) /7 115 27 36 07148 /7 11465 1) 1571946 2192/ 0) 27929 04 11)37 19 742 1411N 141116 29 15928 09 09215 411 11646 54 17742 25 2565/ 15 134 2119II 24 07249 24 11565 /I 15919 14 21922 12 21428 26 11)17 81 342 I4416 1112717 0928 59 09116 2/ 1/74656 17941 34 25752 51 134 210291) 07250 10 11665 411 16218 41 22021 22 IN27 49 11)36 47 342 46 23 NO27 56 06029 50 09416 511 IN46 57 10040 46 2515230 ns 29110 01 07)14 55 11766 0 16418 01 22120 32 IN27 12 11)36 /I 342 41 31 111012141 1161131 41 ON17 32 IN46 56 11119 56 25152 07 113 29230 50 07)5140 11866 16 16717 0 22219 42 21126 /5 1143615 742 44 N nn ON31 12 09518 05 11946 54 18319 06 2595144 02n311 /6 07152 25 11966 27 16917 01 222111 SI 2112510 114/5 59 342 7514 14132 22 09518 )9 14046 51 104/8 16 21451 20 112 294/2 27 07451 10 12066 )6 17116 26 22/18 0/ 28225 22 11435 43 142 I46 51 107N 53 061)311 11%1911 14146 47 111617 26 26050 56 132 295n 16 074515) 12166 42 17415 51 224171) 21224 45 114)5 27 141 4157 110731)1 NI74 04 09619 41 14146 41 187)613 261SO /2 111 M14 05 07554 17 12266 47 17615 16 22416 27 1132414 115)511 141 4713 1106)2 22 1161)4 54 14721 15 1424614 1075 46 26250 07 01 )454 07555 19 12166 49 17914 40 22515 74 21112/ 0 115N 55 741 47 05 ON017 03215 45 1191120 46 14146 26 19014 SS 26249 41 )11 290/5 4) 07556 02 12566 49 18114 04 22614 44 20422 57 11534 SS 341 I* 47 12 NS)3 52 GU)6 )5 SOS21 16 1444616 IN34 05 26149 17 )10 29936 31 07650 41 12666 46 104I) 27 117I) 55 2041121 11514 22 741 77.04 NO 1100apo 017111113 PO 7118114 1.10. MAO NOsookeraniniAl= Ikesamer 7401oea 1110 4717 NS14 37 56237 25 0992146 1444606 19111 14 261411 52 /30 3001211 051137 22 8761515 14166 42 116512/ 240)2 42 26334 06 341 47 21 005/5 22 06231 16 1002213 14545 54 144)2 24 26440 26 )10 30112 42 0193111 07615 56 14266 15 109SO )2 24911 52 25433 49 341 11147 25 N416 17 SO)906 IN22 44 14645 41 19331 0 1654040 129 352I) 14 0)9)901 07716 27 14)6626 NI49 45 250)105 IN31 0 341 4729 NI)652 116119 56 11121 12 14745 27 197/0 42 26547 )4 )29 10311 46 01919 50 0771610 14)66 15 14441157 25130 14 285)317 341 5 47 /2 N3)7 IS 116140 46 10223 )9 14045 11 IN29 52 26647 OS 329 34414 19 0404040 07817 21 1446602 IN40 011 25229 24 285)3 01 141 215 47 35 N3N 23 116141 15 10224 06 14944 SS 20029 01 24646 42 sn 311514 51 0404110 11781710 14565 47 191147 20 25328 /3 28532 44 341 nt4710 SO31101 06442 25 10)24 )2 14944 )7 18120 10 16746 15 1111 NG15 24 04042 21 070IS 27 14665 30 20146 /I 25327 46 216/2 25 341 47 411 On39 SS 46441 13 1042410 1504419 20127 19 26745 40 328 30715 57 04141 09 0791155 14665 11 20145 42 23416 57 206)212 741 4744 N20411 6644454 10425 21 1514359 V 3262/ 261145 21 125 2%16)0 NI41 59 879192) 14764s0205445) 2552601 287)156 141 11147 41 50141 26 66444 51 10325 47 15241)S 2"*25 /11 261144 34 125 NV17 04 04144 49 17319 51 141164 27 ..744 04 25625 28 26731 39 )41 47 44 50142 12 06545 42 IN26 10 15)4)16 20624 47 26944 27 125 31017 IS 04245 )9 NO20 17 14964 03 20941 15 24624 /I 287312) 1411 47 45 NI42 511 66546 )1 10726 11 15442 N 10723 56 27041 59 /27 31115 12 N246 29 NO20 41 IN0011142 25 2572/ 41 2011117 642 47 46 ON41 44 00547 aO 10726 SS 15542 30 Ng2) 05 2704) /2 127 312Hi 46 04247 20 ON2114 15063 10 21/41)6 IN22 54 21431 51 342 47 46 NO44 JS HS411 01 10527 16 15642 05 21122 14 2714) 04 327 31319 10 04/4010 1111121 34 15162 42 21540 46 25822116 21930 /5 642 10 45 36945 16 HS411 56 10927 37 1574140 21121 21 17141 17 )27 31419 55 04/49 00 NI2110 15262 12 21719 56 25921 111 2193019 342 IOU VW 01100 147201 MCA WU. 440. UNA kool MOH *NUM WM/ HISS 0u10 IS 14 03146 0) KS11 30 09227 S7 15141 1) 2124) 06 26042 MI )27 31310 )0 04)2) 04 87616 52 12122 22 13)6146 21968 N 29))113 342 13 53 NI4649 06620 21 09225 16 159441 46 21342 16 26141 41 127 3162105 N4215) 17617 64 12622 45 IN61 05 22159 21 11124 47 142 all 31 NI47 35 06621 12 NJ20 14 IN40 17 21441 26 26141 I) 127 3172140 04424 4) 07718 15 1262) 87 IN60 34 22210 14 2912911 342 17 I) 115240 22 06622 51 19325 51 161/11411 21540 )6 262411 45 /27 311422 15 N425 12 0771150 127212/ 15559 59 22457 411191n 15 342 127 53 On49 11111 06622 54 119429 05 16119 15 216)9 45 2624017 126 31 22 51 04426 22 07119 17 12821 49 15659 2/ 22557 01 2913159 NI 25 /3 0314155 0662144 119419 24 16218 411 218)5 55 26319 49 126 32523 26 04527 12 0702117 12824 10 15710 47 2275014 19121 44 742 14 1) 11250 41 N424 15 NS19 )1 16131 16 21935 N 264)9 21 326 3224 02 04525 12 S/9n 54 12924 29 1585014 22855 27 29120 25 342 19 54 85151 20 06625 26 09629 5) 164)744 IN17 14 26431 SE 126 24 0 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FIGURE140.LAT 32'N.

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FIGURE 141.LAT 26'N.

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ZPC TABLE 6- CORRECTION(9)FORPOLARIS

L.H.A. L.H.A. L.H.A. L.H.A. L.H.A. L.H.A. L.H.A. L.H.A. M Q rr Q 14 Q m Q rr Q rr Q rr Q rr Q I 0 0 I 0 ' OP 0 f OP P OP 35816 53 17 P zz6 so 147 13 192 56 272 at 304 07 -41 -31 t 21 +47 335 51 0 20 117 aq +25 84 45 148 30 196 40 273 49 305 17 -41 -3o . 4 t 22 +48 337 13-28 2 3o 86 za 2 to 34 249 48 201 275 08 306 26 338 37 -43 ao 3 4 33 +49 +23 449 no 49 zsz o7 3 -29 -44 38-3a 224 44 276 27 307 j6 340 03 - 24 +48 +22 4 -30 89 01 zao 58 252 36 229 35 740 -27 I -r25 277 45 308 46 341 30 zo o6-45 +47 +21 5 -31 go a4 122 oll 153 47 233 to 279 02 -46 -26 0 -26 +40+46 4-20 309 342 58 13 13 123 18 - 6 -32 91 45 155 09 236 38 ago AI 312 o5 344 19 -47 -25 + 1 i 27 .+45 -19 26 54 93 16 114 27 239 to 7 -33 4- 156 32 Az 33 312 15 146 04 -48 -14 - 25 4 44 4-15 8 a1 41 125 37 -34 94 15-23 + 3 157 57 141 49 ala 48 313 26 347 37 -49 T29 +43 +17 _, 9 -35 44 34 95 43 120 47 159 23 244 to 184 Oa 314 30 -46 -22 + 4 +30 +42 +16 -10 349 14 49 21 160 51 -36 97 00 246 32 all5 26 315 47 350 55 -47 -21 -I '31 53 oa 137 56 5 +41 +15 -II -37 91-' 17-ao zaq 06 zfra ao 348 s7 alb aq 3to sx 353 39 -46 + 6 +32 -r 40 +14 -11 -38 56 09 99 32 230 16 163 52 aso 36 287 41 3ta zo -45 -19 + 7 +33 +13 -13 354 17-39 58 55 100 47 231 26 165 25 252 to+3 I aS8 53 310 21 -44 -18 + 8 +34 +38+33 +12 356 19 62 36 102 02 167 oz -14 -40 -43 -17 132 37+ o 254 08 290 05 310 34 358 26 63 45 +35 +37 + II -15 -41 103 15 133 48 168 40 255 53 aqz 16 -42 -16 + w +36 +36 311 46 020 65 53 +io -16 -42 104 29 134 59 17011 257 35 19127 323 00 a 30 -41 -Is +II +37 +35 + g -17 -43 67 59 105 41 136 zo 259 14 293 38 324 13 449 -40 _. -14 + IR 17107+33 +34 + 8 -18 -44 69 56 10 54 137 23 173 56 0-`"10 50 294 49 325 28 720 -39 -13 +13 +39 +33 + 7 -19 -45 71 48 108 05 238 34 175 49 210" 23 aos 50 to 46 -38 -12 +14 +40 +33 326 43 109 17 + 6 -20 -46 73 36 139 46 177 41 103 55 297 09 327 58 -37 -II +15 +41 +31 + 5 -21 13 13-47 7510 110 28 140 59 179 53 365 14 298 19 319 15 16 54 -36 io +16 -r30 77 oz +42 +4 -22 -411 zu 39 143 13 283 05 166 52 299 28 -35 9 +17 +43 +20 + 3 330 32-33 a1 41 0 33 112 49 143 27 184 26 368 III 300 38 331 so -49 -34 - 8 +18 +44 +38 44 34 So 13 114 oo + a -24 -48 144 42 286 59 169 43 301 48 333 09 +19 +45 +27 + 1 -25 491 ix gi-33 115 zo 7 145 57 169 47 371 416 -47 -32 6 +20 +40 +2_6 344 37 0 53 03 113 17 116 20 334 34-26 -46 147 13 192 56 372 all 304 07 335 51 56 09

The above table, which does not include refraction, gives the quantity Qo be applies the corrected sextant altitude of Polaris to give the latitude of the observer. In criticalcues ascend. Polaris: Mag. 2.1, S.H.A. 326° 52', Dec. N.89° 10'

TABLE 7- AZIMUTH OFPOLARIS

Latitude LHA. L.H.A. Latitude T 00 300 300 550 600 T o° 50° se 6o° 65°

0 0 . 0 0 , 0 0 0 0 0 0 0 0.5 0.5 0.7 08 0.9 P1 1.4 ISO 359'5 359'5 359'3 359'2MI 3590 3581 20 0.3 0.4 f 0.5 0.6 0.7 0 8 1 o zoo 359'7 359'6 359'5 359'4359'4 359'3 359.1 20 as 0.2 0.3 0.3 0.4 0.5 o.6 '00 359 8 359'8 35S 7 359 7359'6 3596 3591 30 ov 01 0.1 0.1 0.1 01 01 ato ov 359 9 359'0 359'9359'9 359'9 3:19 40 3591 3591 1 35911 35941 35941 359 8 359 7 220 WI WI 02 0-2 0.2 0.2 01 50 359.8 359.7 3596 359 3591 359 4 359 3 230 0.2 o 3 0 4 0.4 0.5 0.5 0.7 60 359'6 359'6 359'4 3591359'2 359 1 358 9 240 04 0.4 0 6 43.6 0.7 0.9 1.3 70 359'5 359'4359'2 359'1359'0 35841 358'5 250 0 5 06 05 08 Iv 1.1 1.4 SO 359'4 3591 359'1 358'935813581 358.3 a6o 0.6 0.7 0.9 Iv 1.2 1.4 1.7 90 3591 359'2 35813581358 6 358'3 357'9 270 01 o 8 1.1 1.2 1.4 IV 2.0 ROO 359.1 359.1 358.8 3581358.5 358 2 357.7 alio 0.8 o 9 l'i 1.3 1.5 141 1'2 120 359.2 359.1 3517 358'6358'4 358'1 3574 200 o8 0.9 Ps 1.4 1-6 1'9 23 120 359'2 3590 3581 358'6358 4 3580 357.6 300 0.8 1 0 1.3 1.4 1.6 14 24 no 359'2 359'1 3581 310 358 358'43511 357.6 08 0.9 1.3 1.4 1'6 1 2'4 ago 359'2 359'1 3581 358'6358'4 358'1 357'7 330 o.8 0.9 1.2 1.4 1.6 iv 2.3 Ego 359'3 359'2 358'9 358'73581358'3 3571 330 07 0.9 1'1 1'3 11 1.8 2.2 160 359'3 359'23590 358'9358'73581 358'1 340 43.7 0.8 1.0 1.2 1.3 1.6 2.0 359'4 170 359'41 359'1 359'0358'9358'7 3514 350 cr6 0.7 cro zv 1.1 1.4 1.7 A* 3591 3591 359'3 359'2 359'1 354'0 358'7 360 01 01 0.7 0.8 0.9 1'1 P4 When Cassiopeia is left (right), Poloru is west (east)

FIGURE 143.-Polaris Correction.

343 132 Appendix 3

TABLE SREFRALTION TO BE SUBTRACTED FROM SEXTANT ALTITUDE

R (a) Height inthousands of feet R

0 10 252025 303540 455055

909090 909090 909090 909090 0 0 63S9 SS 514641 3631 26 20 1713 332926 22 19 16 14 It 10 10 10 a a 21 19 16 14 12 10 Jo Jo 3 161412 to10 3 4 12 1I 10 4 5 1010 5

(b) Height in thousands of metres

I 2 4 5 0 7 S 910 II 221314IS 2617Ig19

90909090 90909090 90909090 90909090 90909090 0 63615855 S3 S04643 2023 17 I 4037 3330 20 1513 II 10 I 33 31 28a6 2421 19 17 16 14 12II 10 10 10 10 1010 10 2 a 21so18 16 15 13 12 1 10101010 3 1413 12 II1010 10 3 4 :2IIto10 10 4 toto

Choose the column appropriate to height, in units of 1000 feet in table 8(a)6: in units of woo metres in table 8(b), and find the range of altitud in which the sextant altitude lies; the corresponding value of R is therefraction to be subtracted from the sextant altitude.

TABLE 9 CORIOLIS (Z) CORRECTION

STANDARD DOME Ground Latitude Ground speed BUBBLE REFRACTION speed SEXTANT knots to°10° 20.30 6o° 70° 40. so llo go° knots ERROR To benetractel from sextant altitude when using Sextant No. so 0 0 0 1 1 1 1 I 1 1 50 sextant suspensionina too 0 0 1 1 2 2 2 2 3 3 zoo perspex dome. tee o 1 1 2 3 3 3 4 4 4 250 200 0 I 2 3 3 4 5 5 S S 200 Alt. Corr. Alt.Refn. Alt.Refn. 250 0 1 2 3 4 5 6 6 6 7 ago 300 0 i 3 4 5 6 7 7 8 8 300 10 8 S0 4 350 o 2 3 5 6 7 8 9 9 9 350 400 0 2 20 7 60 4 4 5 7 8 9:o 10 10 400 450 0 2 4 6 8 9 10 11 12 12 450 3o 6 70 3 500 0 2 4 7 8 10 i i 12 13 13 500 8o 40 5 3 5 5 0 0 3 3 7 9I I 12 14 14 14 530 600 0 3 5 3 Is12 14IS 10 16 600 This table must not be 650 0 3 used if a calibration table is 6 9 II i 13 isi6 17 17 650 700 0 3 6 9 1214 1617 1818 700 fitted to the dome, or if a 750 0 3 7 10 13 15 17 A 1920 750 flat glass plate is provided, 800 0 4 710 13 16 18 20 21 21 Soo or for nonstandard domes. Igo 0 4 8 1I 1417 1921 2222 850 900 0 4 8 12 IS 18 2022 2324 900 Apply by mov ng the pation line a distance Z to starboard (right) of the track in northern latitudes, and to port (left) in southern latitudes.

FIGURE144.Refraction and Coriolis.

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SO 1 2 23 4 56 7 1 9111 121213 141516171811 1903212222232125027262829 , 31 33 3233 343536 21 03639 .4142424344454647484849 SO 51 1 2 33 4 56 7II 9 111 12131414151617 181920 2021 on242326Nff 2829 303131 UU343596371731139404142424344434047484849 305151 S2 1 2 33 4 S6 7 09101011 12 13141516161716193021nonnose27 28292930 31gnuOS3 3637 AO40 41 42434443464248 deSO 51 52 S3 1 2 34 4 56 7 II9101111 12131413017 111919302122233425 262627282930 31 0343435 36 37360041 42.434445464704949505152 553 54 1 2 34 4 56 7 09101112 131414151817 18 192021 22222124ono260 3031 32 33 34353637 3839404041 42 4443464748030 30 515233 54 SS 1 2 34 S 19.6 7 I9 10 1112 131413161617 11 1910 2122nos26 V 2112929 3031 32 34 33 31137 38 363940 4142 43 45 46 4748 49 SO50 51 5253 54 55 56 1 2 34 S 07 7 89101112 131413161711192021 21 2223 24 251627 212930 3132 33 353536370040 41424344 46474849493051 52535455 56 57 1 2 34S 67 8 910 10 1112 13 1413 16 1711 19 X21 22 2331 25 26V 21 2129 30 3132 33 35 36 3738 39 4041 42 4344 45 47 48 4849 50 5152 53 5455 56 5 57 38 1 2 34 5 67 8 910 11 1213 141413 16 1711 19 X21 22 2324 23 2627 28 2930 31 3233 34 36 37 3839 0 4142 43 4444 45 47 48 4950 31 5253 54 5556 57 58 39 1 2 34 S 67I9310111213 14151617 1011930212223 2425262728299130 31 313334 36 37 38390414243 444346448495051 52 5354 55%5758 59

FIGURE 152.Tabulated Altitude Correction Table.

359 360 Appendix 3

TABLE 1.Altitude Correction for Change in Positionof Observer

Correction for 4 Minutes of Time

Rel. Ground Speed in Knots Rel. Zn Zn 50 100 1 . 200 250, 300350 400 4. SOO 550 600650700750SOO 850 900 s 000 +3 +7 +10 +13 +17 +20+23 +27 +. +33 +37 +40+43 +47 ++53 +57 + 000 005 3 7 1 13 17 20 23 27 33 37 43 46 . 53 56 . 355 010 3 7 1. 13 16 20 23 26 30 33 36 39 43 46 49 53 56 350 015 3 6 13 I, 16 19 23 26 32 35 39 42 45 48 52 SS S8 345 020 3 6 13 16 19 22 25 2 31 34 38 41 44 47 SO 53 56 340 025 3 6 12 15 18 21 24 27 30 33 36 39 42 4 42 51 54 335 030 +3 +6 ++t2 +14 +17+20 +23 ++29 +32 +35+38 +40 +43+46 +49 +52 330 035 3 S 6 11 14 16 19 22 25 27 30 33 35 36 41 44 46 49 325 040 3 S 6 10 13 15 16 20 23 26 28 31 33 36 38 41 43 46 320 045 2 5 7 9 12 14 16 19 21 24 26 26 31 33 35 38 40 42 315 050 2 6 9 11 13 15 17 19 21 24 26 28 30 32 34 36 3 310 055 2 4 6 8 10 11 13 15 17 19 21 23 25 27 29 31 33 34 305 060 +2 +3 +5+7 +6 +10+12 +13 +15+17 +18 +20+22 +23 +25+27 +26 +30 300 065 1 3 4 6 7 6 10 11 13 14 15 17 18 20 21 23 24 25 295 070 1 2 3 5 6 7 8 9 10 11 13 14 15 16 17 16 19 21 290 075 1 2 3 3 4 5 6 7 6 9 9 10 11 12 13 14 15 16 265 OW 1 1 2 2 3 3 4 5 5 6 6 7 8 8 9 10 1. 280 ON +0 +1+1 +1+1+2+2 +2 +3+3 +3 +3+4 +4 +4+5 +5 +5 275 090 0 0 . 0 0 0 0 0 0 0 0 0 0 0 . 0 0 0 270 095 0 1 1 1 22 2 33 3 34 4 45 5 5 265 100 1 1 2 2 3 3 4 5 5 6 6 7 8 8 9 9 10 1. 260 105 1 2 3 3 4 5 6 7 8 9 9 10 11 12 13 14 15 16 255 110 1 2 3 5 6 7 6 9 10 11 13 14 15 16 17 16 19 21 250 115 1 3 4 6 7 6 10 11 13 14 15 17 16 20 21 23 24 25 245 120 2 3 5 7 8 10 12 13 1S 17 16 20 22 23 25 27 28 30 240 125 2 4 8 10 1113 15 1719 21 2325 27 2931 33 34 235 130 2 4 9 11 13 15 I.I. 21 24 26 28 30 32 34 36 39 230 135 2 5 7 9 12 14 16 19 21 24 26 26 31 33 35 36 40 42 225 140 3 5 8 10 13 15 15 20 23 26 26 31 33 36 36 41 43 46 220 145 3 5 11 14 16 19 22 25 27 30 33 35 38 41 44 46 4 215 150 3 6 12 14 17 20 23 26 29 32 35 36 40 43 46 49 52 210 155 3 6 12 15 1821 24 2730 33 3639 42 442 Si 54 205 1130 3 6 13 16 19 22 25 26 31 34 36 41 44 47 SO 53 200 165 3 6 1. 13 16 19 23 26 29 32 35 39 42 45 48 52 SS 58 195 170 3 7 1 . 13 16 20 23 26 30 33 36 39 43 46 4 53 36 190 175 3 7 1 13 17 . 23 27 30 33 37 40 43 46 . 53 56 . 185 120 3 7 1013 17 2023 27 3033 37 4043 47 5053 57 60 180

Timeof fix (tab 1) Sign from Toobserved To tabulated To or computation (tab 2) 4.min.Table altitude altitude Intercept

Later than + Add Subtract Toward observation Subtract Add Away Earlier than + Subtract Add Away observation Add Subtract Toward

FIGURE 153.Altitude Correction for Position Table.

361

142 mcKsoNVIII

ILLI sw

FIGURE 154.Navigation Chart. 362 363 FIGURE 155.Navigation Chart. FIGURE 1513.Navigation Chart. 366 367