Cessna 152 Checklist Preflight
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Aero Twin, Inc. STC for Rudder Gust Lock
-- ST02540AK Aero Twin, Inc. 2403 Merrill Field Drive Anchorage, AK 99501 A43EU Airbus Defense and Space S. A. C-212-CB, CC, CD, CE, CF, DF, DE Fabrication and installation of Aero Twin, Inc., Rudder Gust Lock Kit No. 4111-212 on Airbus Defense and Space S. A. C-212 aircraft in accordance with Aero Twin, Inc., Master Data List No. 4111-212-MDL, Original Issue, dated May 8, 2020, or later FAA approved revision. : 1. The compatibility of this design change with previously approved modifications must be determined by the installer. 2. If the holder agrees to permit another person to use this Certificate to alter the product, the holder shall give the other person written evidence of that permission. 3. Instructions for Continued Airworthiness, Aero Twin, Inc. document number 4111-212-ICA, Original Issue, dated May 8, 2020, or later FAA accepted revision is a required part of this modification. 4. Airplane Flight Manual Supplement (AFMS), Aero Twin Doc. No. 4111-212-AFMS, Original Issue, dated August 27, 2020, or later FAA approved revision is a required part of this modification. November 20, 2017 September 8, 2020 _______________________________________________________ (Signature) August A. Asay Manager, Anchorage Aircraft Certification Office _______________________________________________________ (Title) _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES This certificate may be transferred in accordance with FAR 21.47. INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate. -
MGB Alternator Conversion Installation Instructions for MGA & 1962 to 1967 MGB PART# 130-078, 130-088, 130-098 440 Rutherford St
MGB Alternator Conversion Installation Instructions For MGA & 1962 to 1967 MGB PART# 130-078, 130-088, 130-098 440 Rutherford St. Goleta, CA 93117 1-800-642-8295 • FAX 805-692-2525 • www.MossMotors.com Scan the code to watch Moss's Generator to Alternator Conversion Video Or search “Moss TV generator to alternator conversion” on YouTube. Tools required: Vehicle Preparation: Positive Ground to Negative Ground Conversion • Small and medium flat blade screwdriver 1. Remove the battery cover behind the seats using a • Phillips head screwdriver screwdriver to release the dzus fasteners. Disconnect and remove the battery, or both batteries if still • 11/32" wrench, 7/16" wrench, 1/2" wrench, configured for a dual 6 volt set up, using a 1/2" 5/8" wrench wrench. • 7/16" socket with extension, 1/2" socket, 5/8" socket, 22mm socket 2. Disconnect the Yellow/Green and Yellow wires from the generator. If the generator uses ring type • Center punch connectors use a 5/16" and 7/16" wrench. • Hammer 3. For the installation of the Lucas alternator the ignition • 1/4" drill bit, electric drill coil will have to be relocated to the engine bay side • Deadblow hammer of the right fender well. Remove the coil from the generator using a 7/16" socket. Locate a new place • Air impact gun for the coil and mark the hole locations. Using a • Pry bar center punch and hammer, make two dimples at the center of the marks to insure that the drill bit will not • Wire cutters walk around when the holes are being started. -
NTSB/AAB-88/11 I PB88-916911 4 Ai~~~Kfta'a~C1'tfeti~T\N-Iefs - Brief Format U.S
JACK R. HUNT MEMORIAL LIBRARY DAYTONA BEACH, FLORIDA 32014 • 904-239-6595 TECHNICAL REPORT DOCUMENTATION PAGE 1. Report No. 2.Government Accession No. 3.Recipient's Catalog No. NTSB/AAB-88/11 I PB88-916911 4 Ai~~~kfta'A~c1'tfeti~t\n-iefs - Brief Format U.S. Civil and Foreign Aviation 1987 - 7 6.Performing Organization Calendar Year Issue Number Code 7. Author(s) 8.Performing Organization Report No. 9 Perforro.ir.LQ Qr~a.nizatiDn Name and Address 10.Work Unit No. 8ureau or tie1cruperat1ons National Transportation Safety Board Washington, D.C. 20594 11 .Contract or Grant No. 13.Type of Report and Apprbk~~at%~yr~o General 12.Sponsoring Agency Name and Address Aviation and Air Carrier Accidents Occurring in NATIONAL TRANSPORTATION SAFETY BOARD 1987 in Brief Format Washington, D. C. 20594 14.Sponsoring Agency Code 15.Supplementary Notes 16.Abstract This publication contains selected aircraft accident reports in Brief Format occurring in U.S. civil and foreign aviation operations during Calendar Year 1987. Approximately 200 General Aviation and Air Carrier accidents contai.ned in this publication represent a random selection. This publication is issued irregularly, normally eighteen times each year. The Brief Format represents the facts, conditions, circumstances and probable cause(s) for each accident. File Numbers: 1201 through 1400 17.Key Words 18.Distribution Statement Aviation accident, probable cause, findings, This document is available certificate/rating, injuries, type of accident, type to the public through the operating certificate, flight conducted under, National Technical Infor accident occurred during, aircraft damage, basic mation Service, Spring weather field, Virginia 22161 19.Security Classification 20.Security Classification 21 .No. -
Citation X+ There Is Nothing Faster
CITATION X+ THERE IS NOTHING FASTER Period. Fly the uncontested speed leader up to Mach 0.935 (717 mph) to a max altitude of 51,000 feet, way ahead of your competition. Combining cross-continental range, a technologically advanced flight deck and cabin, and legendary performance makes the Citation X®+ unmatched in more than just speed. Max Range Max Cruise Speed Max Passengers 3,460 nm 528 ktas 12 Useful Load Takeoff Distance 14,769 lb 5,250 ft HIGH-PERFORMANCE BOARDROOM Relax in the wide, reclining seats with plenty of legroom, and enjoy the view through 13 large windows. Exceptional leathers and fabrics, hand-finished hardwoods, and a contemporary vanity and lavatory complete the fit and finish of the Citation X+ cabin. STAY CONNECTED IN FLIGHT Manage cabin lighting, window shades, temperature and entertainment with simple touch-screen commands, and stay connected with in-cabin high-speed Internet and Wi-Fi. AN INTERIOR DESIGNED FOR YOUR NEEDS Thirteen large windows Standard belted Executive tables Additional storage Class-leading Fully tracking, Large galley with flushing lavatory stow neatly between seats legroom berthable room for food swing-out seats preparation CUSTOMIZED COMFORT Choose customized interior finishes and personalized touches throughout to make the Citation X+ your own. Multiple cabin compartments and additional storage space are just a few of the available options. Standard Seating Optional Seating LEADING-EDGE AVIONICS The Garmin™ G5000™ avionics suite allows pilots to individualize their layouts, providing such features as full-dimensional renderings of terrain and precise weather pattern and traffic monitoring, all from a touch-screen, intuitive interface. -
Government Gazette Republic of Namibia
GOVERNMENT GAZETTE OF THE REPUBLIC OF NAMIBIA N$1.56 WINDHOEK- 31 January 1996 No. 1253 CONTENTS Page APPLICATION TO OPERATE AIR SERVICES......................... 1 APPLICATION TO OPERATE AIR SERVICES The following applications for Scheduled Air Transport Services, Non-sched uled Air Transport Services, Flying Training Air Services or Aerial Work Air Services indicate ( 1) reference number; (2) name of applicant and nature of application; (3) number and type of aircraft; (4) nature of proposed air service; and (5) routes over or area within which the proposed air services are to be rendered and are published in terms of section 5 of the Air Services Act, 1949 (Act 51 of 1949) as amended . Representations by interested parties in respect of the applications shall comply with the requirements of section 6 of the Air Services Act, 1949 (Act 51 of 1949) and shall be in ninefold in respect of each - application and shall be delivered by hand or sent by registered post to the ··- Secretary, Transport Commission of Namibia, Private Bag X12005, Windhoek to reach that office not later than 21 days after the date of publication of this Government Gazette . ,,• 2 Government Gazette 31 January 1996 No. 1253 WINDHOEK (1) 07/12/95 OOA00113 (2) KALAHARI EXPRESS AIRLINES -Application for a scheduled air transport service licence. (3) Two Fokker F28 Twin Engined Fan Jet (55 Seater) (4) Types of traffic to be conveyed: Passengers and their personal effects and fast freight. See Annexure D. (5) Area to be served: Namibia and Republic of South Africa. Routes and towns to be served: Windhoek (Eros)- Johannesburg International Airport. -
Leburg Electronic Ignition System EI10A Installation Manual
Leburg Electronic Ignition System EI10A Installation Manual For Aero VW’s - Or Any 2 Or 4 Cylinder 4 Stroke Engine Skycraft Ltd Telephone: 01406 540777 Riverside House Bloodfold Farm Website: www.skycraft.ltd Ravens Bank Saturday Bridge Email: [email protected] Holbeach Lincolnshire Facebook: @skycraftlimited PE12 8SR © Skycraft Ltd 2013 Leburg EI10A Manual—July 2020 Page 1 Contents 1. Read This First 2. The VW As An Aero Engine 3. Ignition System Performance 4. Principles Of Operation 5. Set Up 6. Power Supplies 7. Fitting A Honda CBR 600 Alternator 8. Manufacture & Assembly Notes 9. Wiring Notes 10. Wiring Up The Spark Plugs 11. Drawings © Skycraft Ltd 2013 Leburg EI10A Manual—July 2020 Page 2 1. Read This First By virtue of the techniques, design, components used and the care taken in building and testing, each ignition controller is believed to be highly reliable. The risk of failure is thus low, but it is finite. Therefore, this system is only made available on the basis that the user agrees to implement a Dual Ignition System. The Leburg system is the dual system, with the power supply system described in this manual. If any change from this is intended, you will need to check with the LAA that they will accept it. If a different alternator or power system is used, again, you will need to check with the LAA that they will accept it. The benefits of smooth running and getting the maximum power are obtained when the system is installed as described in this manual, with dual controllers, dual ignition spark plugs, both firing at the same time at the optimum advance angle. -
Before Endine Start
C-A152 CESSNA – NORMAL PROCEDURES BEFORE ENGINE START THROUGH ENGINE SHUTDOWN – CHECKLIST WILL BE VERBALIZED BEFORE ENGINE START WINDOWS ..................................................................................................................... SECURE CABIN DOORS ............................................................................................................. CLOSED TACH TIME ................................................................................... CHECK TIME REMAINING HOBBS TIME ................................................................................................................ RECORD BEFORE TAKE-OFF BRAKES ....................................................................................... APPLY TOE BRAKES ONLY TYPE OF TAKEOFF .............................................................................................. DETERMINE PASSENGER BRIEF ................................................................................................ COMPLETE FLAPS .................................................................................................................. AS REQUIRED SEATBELTS AND HARNESSES .........................................................FASTEN AND SECURE AIRSPEEDS: ROTATION, CLIMB OUT, CABIN DOOR ......................................................................................... CLOSE AND SECURE AND BEST GLIDE ................................................................... CALCULATE (GUST SPREAD) PRE-TAKEOFF BRIEFING ..................................................................................... -
Aviation Maintenance Alerts
ADVISORY CIRCULAR 43-16A AVIATION MAINTENANCE ALERTS ALERT FEBRUARY NUMBER 2006 331 CONTENTS AIRPLANES AVIAT .........................................................................................................................................1 BEECH ........................................................................................................................................2 CESSNA ......................................................................................................................................4 DASSAULT.................................................................................................................................6 GULFSTREAM...........................................................................................................................8 ISRAEL AIRCRAFT.................................................................................................................11 PIPER.........................................................................................................................................13 RAYTHEON..............................................................................................................................15 HELICOPTERS AGUSTA ...................................................................................................................................16 POWERPLANTS PRATT & WHITNEY ...............................................................................................................16 ACCESSORIES AERO-TRIM .............................................................................................................................18 -
Model 162 SERIAL NUMBER
Model 162 SERIAL NUMBER Serials 16200001 and On REGISTRATION NUMBER This publication includes the material required to be furnished to the pilot by ASTM F2245. COPYRIGHT © 2009 ORIGINAL ISSUE - 22 JULY 2009 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA REVISION 3 - 28 SEPTEMBER 2010 162PHUS-03 U.S. CESSNA INTRODUCTION MODEL 162 GARMIN G300 PILOT’S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT CESSNA MODEL 162 SERIALS 16200001 AND ON ORIGINAL ISSUE - 22 JULY 2009 REVISION 3 - 28 SEPTEMBER 2010 PART NUMBER: 162PHUS-03 162PHUS-03 U.S. i/ii CESSNA INTRODUCTION MODEL 162 GARMIN G300 CONGRATULATIONS Congratulations on your purchase and welcome to Cessna ownership! Your Cessna has been designed and constructed to give you the most in performance, value and comfort. This Pilot’s Operating Handbook has been prepared as a guide to help you get the most utility from your airplane. It contains information about your airplane’s equipment, operating procedures, performance and suggested service and care. Please study it carefully and use it as a reference. The worldwide Cessna Organization and Cessna Customer Service are prepared to serve you. The following services are offered by each Cessna Service Station: • THE CESSNA AIRPLANE WARRANTIES, which provide coverage for parts and labor, are upheld through Cessna Service Stations worldwide. Warranty provisions and other important information are contained in the Customer Care Handbook supplied with your airplane. The Customer Care Card assigned to you at delivery will establish your eligibility under warranty and should be presented to your local Cessna Service Station at the time of warranty service. • FACTORY TRAINED PERSONNEL to provide you with courteous, expert service. -
Shooting Down Civilian Aircraft: Is There an International Law Brian E
Journal of Air Law and Commerce Volume 72 | Issue 3 Article 10 2007 Shooting down Civilian Aircraft: Is There an International Law Brian E. Foont Follow this and additional works at: https://scholar.smu.edu/jalc Recommended Citation Brian E. Foont, Shooting down Civilian Aircraft: sI There an International Law, 72 J. Air L. & Com. 695 (2007) https://scholar.smu.edu/jalc/vol72/iss3/10 This Article is brought to you for free and open access by the Law Journals at SMU Scholar. It has been accepted for inclusion in Journal of Air Law and Commerce by an authorized administrator of SMU Scholar. For more information, please visit http://digitalrepository.smu.edu. SHOOTING DOWN CIVILIAN AIRCRAFT: IS THERE AN INTERNATIONAL LAW? BRIAN E. FOONT* TABLE OF CONTENTS PRO LO G U E .............................................. 696 INTRODUCTION ......................................... 697 I. BACKGROUND .................................... 698 A. PRESIDENT TITO'S LETTER ...................... 700 II. SOURCES OF INTERNATIONAL LAW ............ 701 III. POST-WORLD WAR II INCIDENTS ............... 704 A. SOVIET UNION-SHOOT DOWN OF FRENCH COMMERCIAL AIRLINER .......................... 704 B. CHINA-SHOOT DowN OF CATHAY PACIFIC FLIGHT ......................................... 705 C. BULGARIA-SHOOT DowN OF ISRAELI EL AL PASSENGER JET .................................. 705 D. ISRAEL-SHOOT DowN OF LIBYAN AIRLINES PASSENGER JET .................................. 706 E. SOVIET UNION-SHOOT DowN OF KOREAN AIRLINES PASSENGER JET (FLIGHT 902) .......... 707 F. SOVIET UNION-SHOOT DowN OF KOREAN AIRLINES PASSENGER JET (FLIGHT 007) AND ARTICLE 3 BIS TO THE CHICAGO CONVENTION .. 707 G. UNITED STATES-SHOOT DOWN OF IRANIAN AIRLINES PASSENGER JET (FLIGHT 655) .......... 711 * The Law Offices of Brian E. Foont, PLLC; LL.M., Georgetown University Law Center; J.D., American University Washington College of Law; B.A., University of Rochester. -
Citation Sovereign+ Redraw Your Range Map
CITATION SOVEREIGN+ REDRAW YOUR RANGE MAP Range-enhancing winglets combined with powerful engines allow the CESSNA CITATION SOVEREIGN+ aircraft to land on smaller runways and at airports surrounded by obstacles. This reduces travel time and grants access to popular destinations such as Aspen, Hilton Head and Ocean Reef. The sizable cabin makes every business trip a pleasure. Maximum Range Maximum Cruise Speed Maximum Passengers Useful Payload Takeoff Distance 3,200 nm 460 ktas 12 12,794 lb 3,530 ft UNMATCHED INGENUITY CITATION SOVEREIGN+ SPECIFICATIONS INTERIOR Cabin Height 68 in 1.73 m Cabin Width 66 in 1 .68 m Cabin Length 25 ft 3 in 7.70 m TOUCH-SCREEN SPACIOUS CABIN HEATED BAGGAGE AVIONICS The spacious, versatile cabin features COMPARTMENT BAGGAGE CAPACITY electrically operated windows and a Weight 1,435 lb 651 kg NextGen-capable GARMIN double-club seating configuration. The heated baggage compartment can G5000 avionics streamline the hold up to 1,000 pounds and 100 cubic Volume 135 cu ft 3.82 cu m pilot experience with advanced feet of cargo. autothrottles and touch-screen WEIGHTS simplicity. Max Takeoff 30,775 lb 1 3,959 kg Basic Operating Weight 1 8,235 lb 8,27 1 kg Useful Load 12,790 lb 5,801 kg MAX PASSENGERS 12 ENGINES Manufacturer Pratt & Whitney Canada Model (2) PW306D Thrust 5,907 lb 26.28 kN ea PERFORMANCE Takeoff Field Length (MTOW) 3,530 ft 1,076 m Max Range 3,200 nm 5,926 km Max Cruise Speed 460 ktas 852 km/h FUEL-EFFICIENT ENGINES Time to Climb FL 450 in 27 min POWERFUL CLASS-LEADING Pratt & Whitney Canada engines deliver low-cost ELECTRICAL SYSTEM TAKEOFF FIELD LENGTH maintenance, high reliability and fuel efficiency for Performance data is based on standard conditions with zero wind. -
Comment Response Document
EASA SC-VTOL-01 Comment Response Document Note: The comments have been grouped by theme or objective and renumbered sequentially. Bookmarks are available to navigate the document. General type of vehicle Explanatory Note 1: type of vehicle The Special Condition (SC) has been developed to cover a new category of person-carrying vertical take-off and landing (VTOL) heavier-than-air aircraft with lift/thrust units used to generate powered lift and control. The vertical take-off and landing capability distinguishes this type of aircraft from aeroplanes. The Special Condition does not intend to cover traditional rotorcraft either but rather aircraft with distributed lift/thrust and it will be clarified that, for the SC to be applicable, more than 2 lift/thrust units should be used to provide lift during vertical take-off or landing. The Special Condition background mentioned “the aircraft may not be able to perform an autorotation or a controlled glide in the event of a loss of lift/thrust” as it is the case for some VTOL aircraft being proposed, however this is not a requirement. Comment Comment summary Suggested resolution Comment is an Comment is EASA EASA response observation or substantive or comment is a is an NR Author Paragraph Page disposition suggestion* objection** 1 1David Loebl, Background/Sc 1 “Although hover flight may be possible, the aircraft Clarify the condition where no glide is possible: Yes No Noted See Explanatory Note 1 AutoFlightX ope may not be able to perform an autorotation or a “…not be able to perform an autorotation or a controlled glide in the event of a loss of lift/thrust.” controlled glide in the event of a loss of lift/thrust implies that the given SC are not applicable for during hover.” transition vehicles that can fly also with aerodynamic lift.