WEC Aircraft Use and Safety Handbook
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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. -
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. -
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. -
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. -
Garmin Reveals Autoland Feature Rotorcraft Industry Slams Possible by Matt Thurber NYC Helo Ban Page 45
PUBLICATIONS Vol.50 | No.12 $9.00 DECEMBER 2019 | ainonline.com Flying Short-field landings in the Falcon 8X page 24 Regulations UK Labour calls for bizjet ban page 14 Industry Forecast sees deliveries rise in 2020 page 36 Gratitude for Service Honor flight brings vets to D.C. page 41 Air Transport Lion Air report cites multiple failures page 51 Rotorcraft Garmin reveals Autoland feature Industry slams possible by Matt Thurber NYC helo ban page 45 For the past eight years, Garmin has secretly Mode. The Autoland system is designed to Autoland and how it works, I visited been working on a fascinating new capabil- safely fly an airplane from cruising altitude Garmin’s Olathe, Kansas, headquarters for ity, an autoland function that can rescue an to a suitable runway, then land the airplane, a briefing and demo flight in the M600 with airplane with an incapacitated pilot or save apply brakes, and stop the engine. Autoland flight test pilot and engineer Eric Sargent. a pilot when weather conditions present can even switch on anti-/deicing systems if The project began in 2011 with a Garmin no other safe option. Autoland should soon necessary. engineer testing some algorithms that could receive its first FAA approval, with certifi- Autoland is available for aircraft manu- make an autolanding possible, and in 2014 cation expected shortly in the Piper M600, facturers to incorporate in their airplanes Garmin accomplished a first autolanding in followed by the Cirrus Vision Jet. equipped with Garmin G3000 avionics and a Columbia 400 piston single. In September The Garmin Autoland system is part of autothrottle. -
Aircraft Control After Engine Failure on Takeoff
General AviaƟon FAA Joint Steering CommiƩee Aviaon Safety Training Aid January 2016 Aircraft Control After Engine Failure on Takeoff Studies have shown that startle responses during unexpected situaons such as power‐plant failure during takeoff or inial climb have contributed to loss of control of aircra. By including an appropriate plan of acon in a departure briefing for a power‐plant failure during takeoff or inial climb, you can manage your startle response and maintain aircra control. Considerations for Takeoff Brief Best Practices The briefing given by the pilot‐in‐command As part of pre‐planning and preparaon, (PIC) should be specific for each flight. Avoid consider these in case of a power‐plant failure allowing the checklist to become roune and create during and aer take‐off. Addional training and complacency. pracce — in a safe environment with a flight instructor — can reduce the startle response to an Airport Info: Consider runway condions, traffic acvies, and airspace complexies. unexpected event, such as an actual power‐plant failure, and improve outcomes. Idenfy V Speeds: Airspeeds such as Vy, Vx, Vr and best glide should be considered for current Straight Ahead or Turn Back? Research condions prior to takeoff. indicates a higher probability of survival if you connue straight ahead following an engine Terrain/Obstrucons: Mountains, power‐lines, failure aer take‐off. Turning back actually trees or towers may become obstrucons requires a turn of greater than 180 degrees aer during emergencies; idenfy them prior to taking into account the turning radius. Making a departure. turn at low altudes and airspeeds could create Abort Point: Establish an abort point prior to a scenario for a stall/spin accident. -
FAA Order JO 7110.65U, Air Traffic Control
ORDER JO 7110.65U Air Traffic Organization Policy Effective Date: February 9, 2012 SUBJ: Air Traffic Control This order prescribes air traffic control procedures and phraseology for use by personnel providing air traffic control services. Controllers are required to be familiar with the provisions of this order that pertain to their operational responsibilities and to exercise their best judgment if they encounter situations not covered by it. Distribution: ZAT-710, ZAT-464 Initiated By: AJV-0 Vice President, System Operations Services RECORD OF CHANGES DIRECTIVE NO. JO 7110.65U CHANGE SUPPLEMENTS CHANGE SUPPLEMENTS TO OPTIONAL TO OPTIONAL BASIC BASIC FAA Form 1320−5 (6−80) USE PREVIOUS EDITION 2/9/12 JO 7110.65U Explanation of Changes Basic Direct questions through appropriate facility/service center office staff to the Office of Primary Interest (OPI) a. 2−5−2. NAVAID TERMS d. 5−9−10. SIMULTANEOUS INDEPEND- 4−2−1. CLEARANCE ITEMS ENT APPROACHES TO WIDELY-SPACED 4−2−5. ROUTE OR ALTITUDE PARALLEL RUNWAYS WITHOUT FINAL AMENDMENTS MONITORS 4−2−9. CLEARANCE ITEMS 4−3−2. DEPARTURE CLEARANCE This change adds a new paragraph allowing 4−3−3. ABBREVIATED DEPARTURE simultaneous independent approaches to widely CLEARANCE spaced parallel runways separated by 9,000 feet or 4−7−1. CLEARANCE INFORMATION more−without monitors. This change cancels and 4−8−2. CLEARANCE LIMIT incorporates N JO 7110.559, Simultaneous Inde- This change clarifies how to issue clearances that pendent Approaches to Widely-Spaced Parallel contain NAVAIDs and provides new phraseology Runways Without Final Monitors, effective and examples. July 29, 2011. b. -
The Restoration of 1968 Cessna C-150H N22507
The Restoration of 1968 Cessna C-150H N22507 By Mark van Wyk (Updated June 28, 2010) 1 On the cover of this article, there is a before and after comparison of my airplane: a 1968 Cessna C-150H tail number N22507. Maybe it looks pretty much the same now is it did before, but a lot of work was done and a lot of money was spent to upgrade and restore the airplane. Fortunately, it’s been a “flying work in progress,” meaning I was able to fly the plane pretty much the whole time that I was working on it. What inspired me to spend so much time and money fixing up the plane? The first clue that I needed to start thinking about some major re-working happened in November, 2007, when my old engine conked out in Death Valley National Monument, CA on my way to a C-150/152 Club fly-in, about nine miles south of Furnace Creek Airport. The exhaust valve in the #2 cylinder had disintegrated. The vibration and noise was bad, but the propeller continued to turn, and my altitude loss was not too severe. Fortunately, I landed safely, and miraculously, A&P mechanic Mr. Dick Tremaine, who is based in Dyer, Nevada, flew out his C-150, with tools and a spare used cylinder, and he managed to fix the plane, with me assisting, and make it flyable so that I could get home. Mr. Dick Tremain (right) and I (left) Repairing the Old Engine in Death Valley, CA About 100 hours of flying time later, the oil pressure began to drop noticeably, and metal particles were observed in the oil – definite signs that it was time for an engine overhaul – something every airplane owner should be prepared to do when the time comes. -
150/152 Model History the Cessna Pilots Association Educational and Technical Center Santa Maria Public Airport 3940 Mitchell Rd
150/152 Model History The Cessna Pilots Association Educational and Technical Center Santa Maria Public Airport 3940 Mitchell Rd. Santa Maria, CA 93455 805/934-0493 Fax 805/934-0547 www.cessna.org 150/152 History page 1 ©Cessna Pilots Association — July 17, 2006 Model 150 History John M. Frank 1959 - 150 Serial Numbers: 17001 thru 17683 Base Price - $6,995, Average price as Delivered - $8,795 Cessna introduces the model 150 in October of 1958. It is a two place, side by side, all metal, high wing aircraft designed for the trainer market. Initially the Model 150 was offered in three versions, the bare bones Standard, the Trainer, which came with dual controls, brakes landing light, clock, sun visors, outside air temperature gauge, cigarette lighter, turn and bank indicator as well as a Narco Superhomer VOR with nine cyrstals. The Commuter had all of the above plus a vacuum system and attitude and direction indicators. Features of all models include: 1. Tricycle landing gear 2. 40 degree “Para-Lift” flaps 3. Continental O-200 A engine, 100 HP. This engine initially has a 600 hour TBO which was raised to 1800 hours late in the model year 4. 14 volt, 20 amp generator 5. Gross Weight 1500 lbs 6. Fuel Capacity 26 gallons 7. Optional wheel fairings 1960 - 150 Serial Numbers: 17684 thru 17999, 59001 thru 59018 Base Price - $7,250, Average Price as Delivered - $8,950 1. Propeller shortened 2. Larger fuel supply lines beginning at Serial Number 17770 3. Stall warning heat and Pitot heat optional 4. -
Barnett, James Scott OH128
Wisconsin Veterans Museum Research Center Transcript of an Oral History Interview with JAMES S. BARNETT Navy, Airplane navigator and co-pilot, World War II 2000 OH 128 1 OH 128 Barnett, James Scott, (1918-). Oral History Interview, 2000. User Copy: 1 sound cassette (ca. 65 min.); analog, 1 7/8 ips, mono. Master Copy: 1 sound cassette (ca. 65 min.); analog, 1 7/8 ips, mono. Video Recording: 1 videorecording (ca. 65 min.); ½ inch, color. Transcript: 0.1 linear ft. (1 folder). Abstract: James Barnett, a Kenosha, Wisconsin native, discusses his World War II service as an aerial navigator and co-pilot with the Navy. Barnett mentions enlisting in 1942, attending preflight training in Iowa, and learning about navigation and gunnery at the Naval Air Station (Florida). He relates his duties as a crewmember of a PBY squadron in Hawaii. Barnett talks about bombing missions to the Gilbert Islands, Wake Island, and Ellice Island. He recalls how he and two other crew members were grounded with dysentery the day that their plane and the rest of the crew were shot down and killed. Barnett mentions his transfer to New Guinea and missions to the Philippines and Truk. He talks about getting hit in the leg during a bombing run and doing an emergency landing on Kwajalein due to engine damage. Barnett speaks of his return to the United States and being stationed at Kaneohe Bay (Hawaii). He describes losing a plane due to landing gear malfunction. He talks about flying from San Francisco to Hawaii in nine hours and judging whether to turn around using “how-goes-it” curves. -
(VL for Attrid
ECCAIRS Aviation 1.3.0.12 Data Definition Standard English Attribute Values ECCAIRS Aviation 1.3.0.12 VL for AttrID: 391 - Event Phases Powered Fixed-wing aircraft. (Powered Fixed-wing aircraft) 10000 This section covers flight phases specifically adopted for the operation of a powered fixed-wing aircraft. Standing. (Standing) 10100 The phase of flight prior to pushback or taxi, or after arrival, at the gate, ramp, or parking area, while the aircraft is stationary. Standing : Engine(s) Not Operating. (Standing : Engine(s) Not Operating) 10101 The phase of flight, while the aircraft is standing and during which no aircraft engine is running. Standing : Engine(s) Start-up. (Standing : Engine(s) Start-up) 10102 The phase of flight, while the aircraft is parked during which the first engine is started. Standing : Engine(s) Run-up. (Standing : Engine(s) Run-up) 990899 The phase of flight after start-up, during which power is applied to engines, for a pre-flight engine performance test. Standing : Engine(s) Operating. (Standing : Engine(s) Operating) 10103 The phase of flight following engine start-up, or after post-flight arrival at the destination. Standing : Engine(s) Shut Down. (Standing : Engine(s) Shut Down) 10104 Engine shutdown is from the start of the shutdown sequence until the engine(s) cease rotation. Standing : Other. (Standing : Other) 10198 An event involving any standing phase of flight other than one of the above. Taxi. (Taxi) 10200 The phase of flight in which movement of an aircraft on the surface of an aerodrome under its own power occurs, excluding take- off and landing. -
FTW-8G Emergency Approach and Landing
FTW-8G Emergency Approach and Landing READING ASSIGNMENT Pilot’s Operating Handbook, Emergency Procedures, Engine Failures AFH Pages 8-26 to 8-27 – “Emergency Approaches and Landings (Simulated)” Study Questions Pilot’s Operating Handbook, Emergency Procedures, Engine Failures 1. In the Emergency Procedures section of a POH, what is typically indicated by emergency procedure steps FTW-8G ? that are shown in boldface type? a) The steps should be memorized. b) The steps are optional. c) Additional information regarding those steps is contained in the amplified procedures section of the POH. 2. Why are the emergency procedures for dealing with an engine failure just after takeoff different from the procedures for dealing with an engine failure in flight? a) The best glide airspeeds are significantly different and result in very different glide angles. b) Engine failures at altitude may allow time for restart procedures to be attempted. c) If the wheels have not stopped spinning from the takeoff roll, the aerodynamics of the forced landing will be substantially different. 3. When responding to an engine failure immediately after takeoff, or for any forced landing, why is it a good idea to shutdown and secure the engine prior to landing? a) Having the engine on limits the effectiveness of flaps and ailerons. b) To reduce the possibility of a post-crash fire. c) To reserve some fuel for future takeoffs, if needed. 4. When should the airplane’s avionics and electrical system be shut down during a forced landing? a) Once landing is assured. b) Prior to squawking 7700 on the transponder.