AIR-TECH Complete Manual
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Easy Access Rules for Auxiliary Power Units (CS-APU)
APU - CS Easy Access Rules for Auxiliary Power Units (CS-APU) EASA eRules: aviation rules for the 21st century Rules and regulations are the core of the European Union civil aviation system. The aim of the EASA eRules project is to make them accessible in an efficient and reliable way to stakeholders. EASA eRules will be a comprehensive, single system for the drafting, sharing and storing of rules. It will be the single source for all aviation safety rules applicable to European airspace users. It will offer easy (online) access to all rules and regulations as well as new and innovative applications such as rulemaking process automation, stakeholder consultation, cross-referencing, and comparison with ICAO and third countries’ standards. To achieve these ambitious objectives, the EASA eRules project is structured in ten modules to cover all aviation rules and innovative functionalities. The EASA eRules system is developed and implemented in close cooperation with Member States and aviation industry to ensure that all its capabilities are relevant and effective. Published February 20181 1 The published date represents the date when the consolidated version of the document was generated. Powered by EASA eRules Page 2 of 37| Feb 2018 Easy Access Rules for Auxiliary Power Units Disclaimer (CS-APU) DISCLAIMER This version is issued by the European Aviation Safety Agency (EASA) in order to provide its stakeholders with an updated and easy-to-read publication. It has been prepared by putting together the certification specifications with the related acceptable means of compliance. However, this is not an official publication and EASA accepts no liability for damage of any kind resulting from the risks inherent in the use of this document. -
Exec Summary (PDF)
BEECHCRAFT® AT-6 The Future of Light Attack is Here. Capable. Affordable. Sustainable. Interoperable. One platform with multiple missions: initial pilot training, weapons training, operational NetCentric ISR and Light Attack capabilities for irregular warfare. The Beechcraft AT-6 is a multi-role, multi-mission aircraft system designed to meet a wide spectrum of warfighter needs: • Based on the proven Beechcraft USAF T-6A and USN T-6B • Designed to accommodate 95% of the aircrew population; widest range in its class • Lockheed Martin plug-and-play mission system architecture adapted from A-10C • Sensor suite adapted from the MC-12W • Flexible, reconfigurable hardpoints with six external store stations Unparalleled attributes with • Long persistence with two aircrew and weapons; up to 1,485 nm self-deployment range a wide range of options. • Extensive variety of weapons including general purpose, laser guided and inertially-aided munitions AIRFRAME AND POWERPLANT • 1,600 shaft horsepower engine • The only fixed-wing aircraft to fire laser guided rockets • ISR suite and six external store hardpoints • Light armor COMBAT MISSION SYSTEMS • Mission systems by Lockheed Martin • NVIS cockpit • Helmet-mounted cueing system • Infrared missile warning and countermeasures COMMUNICATIONS SUITE • Secure voice and data • Rover-compatible full motion video • SADL/Link-16 compatible • SATCOM ISR SUITE • MX-15Di WEAPONS INTEGRATION • 17 60 capable stores management system • .50 Cal Gun • 20mm Gun • 250/500 lb. laser guided GPS or GP bombs • Laser guided missiles • Laser guided rockets • Small 1760 weapons Learn more. Call +1.316.676.0800 or visit Beechcraft.com 13LSAT6HW Specifications and performance are subject to change without notice. -
Air Force Airframe and Powerplant (A&P) Certification Program
Air Force Airframe and Powerplant (A&P) Certification Program Introduction: Most military aircraft maintenance technicians are eligible to pursue the Federal Aviation Administration (FAA) Airframe & Powerplant (A&P) certification based on documented evidence of 30 months practical aircraft maintenance experience in airframe and powerplant systems per Title 14, Code of Federal Regulations (CFR), Part 65- Certification: Airmen Other Than Flight Crew Members; Subpart D-Mechanics. Air Force education, training and experience and FAA eligibility requirements per Title 14, CFR Part 65.77. This FAA-approved program is a voluntary program which benefits the technician and the Air Force, with consideration to professional development, recruitment, retention, and transition. Completing this program, outlined in the program Qualification Training Package (QTP), will assist technicians in meeting FAA eligibility requirements and being better-prepared for the FAA exams. Three-Tier Program: The program is a three-tier training and experience program. These elements are required for program completion and are important for individual development, knowledge assessment, meeting FAA certification eligibility, and preparation for the FAA exams: Three Online Courses (02AF1-General, 02AF2-Airframe, & 02AF3-Powerplant). On the Job Training (OJT) Qualification Training Package(QTP). Documented evidence of 30 months practical experience in airframe and powerplant systems. Program Eligibility: Active duty, guard and reserve technicians who possess at least a 5-skill level in one of the following aircraft maintenance AFSCs are eligible to enroll: 2A0X1, 2A090, 2A2X1, 2A2X2, 2A2X3, 2A3X3, 2A3X4, 2A3X5, 2A3X7, 2A3X8, 2A390, 2A300, 2A5X1, 2A5X2, 2A5X3, 2A5X4, 2A590, 2A500, 2A6X1, 2A6X3, 2A6X4, 2A6X5, 2A6X6, 2A690, 2A691, 2A600 (except AGE), 2A7X1, 2A7X2, 2A7X3, 2A7X5, 2A790, 2A8X1, 2A8X2, 2A9X1, 2A9X2, and 2A9X3. -
Fly-By-Wire - Wikipedia, the Free Encyclopedia 11-8-20 下午5:33 Fly-By-Wire from Wikipedia, the Free Encyclopedia
Fly-by-wire - Wikipedia, the free encyclopedia 11-8-20 下午5:33 Fly-by-wire From Wikipedia, the free encyclopedia Fly-by-wire (FBW) is a system that replaces the Fly-by-wire conventional manual flight controls of an aircraft with an electronic interface. The movements of flight controls are converted to electronic signals transmitted by wires (hence the fly-by-wire term), and flight control computers determine how to move the actuators at each control surface to provide the ordered response. The fly-by-wire system also allows automatic signals sent by the aircraft's computers to perform functions without the pilot's input, as in systems that automatically help stabilize the aircraft.[1] Contents Green colored flight control wiring of a test aircraft 1 Development 1.1 Basic operation 1.1.1 Command 1.1.2 Automatic Stability Systems 1.2 Safety and redundancy 1.3 Weight saving 1.4 History 2 Analog systems 3 Digital systems 3.1 Applications 3.2 Legislation 3.3 Redundancy 3.4 Airbus/Boeing 4 Engine digital control 5 Further developments 5.1 Fly-by-optics 5.2 Power-by-wire 5.3 Fly-by-wireless 5.4 Intelligent Flight Control System 6 See also 7 References 8 External links Development http://en.wikipedia.org/wiki/Fly-by-wire Page 1 of 9 Fly-by-wire - Wikipedia, the free encyclopedia 11-8-20 下午5:33 Mechanical and hydro-mechanical flight control systems are relatively heavy and require careful routing of flight control cables through the aircraft by systems of pulleys, cranks, tension cables and hydraulic pipes. -
S-6S Text Manual
0or* -- *IF9 S-6s COYOTE II 1 16WING HAYS, KS 6760 1 (7.51 625-6346 DESIGNED BY: RANDY SCHLITTER Your manual is ready for assembly: 1. Place the technical manual in the larger 3 ring binder and the parts manual in the smaller 3 ring binder. Every page has a section number then a page number within that section. (Example: parts page 13-02) Parts pages have an exploded view and a parts listing. Text pages are assigned with the prefix "0". 2. Separate the sections with the tab inserts listed below. Follow the table of contents for the order that the manual should follow. 3. Cut out and slip in the labels to corresponding sections. -------r------ -I------- T - - 1 GENERALDATA S-1 FIREWALL DOORS -wyNi- I I I I I I I I I I I I I GENERAL DATA I S-1 FIREWALL I DOORS I WINGS I OPTIONS I -r------1 - FuLLAOE - EN; NE -wTNisiEL - TilZ I' I MOUNT I I LsGMsLY I I I I I I I I r-------r-( FUSELAGE I ENGINE------I------- MOUNT I WINDSHIELD I TRIAL ASSEMBLY I I -r------1 MAIN GEAR TAILCONE BATTERY Box - - I I I I I I I I I I I I ( MAlN GEAR 1 TAILCONE I BATTERY BOX I COVERING I I ----- l- - - - - - - l- - - - - - - -I- - - - - - - 1-------1 -NOSE GEAR, CONTROL STICK SEATISEAT BELT PAINTING I TAILWHEEL I I I I I I NOSE GEAR1 1 I 1 I I ( TAILWHEEL I CONTROL STICK I SEATISEAT BELT I PAINTING I I FLOoiBiAiD; - TNTERIO; - T--T~L-- lNZisSEMBLY -r------l I RUDDER PEDAL I I I I I I FLOORBOARD1 I I I I I ...........................I RUDDER PEDAL I INTERIOR I TAIL I FINAL ASSEMBLY--------- I I RANS, RANS, INC. -
For Improved Airplane Performance
BLENDED WINGLETS FORFOR IMPROVEDIMPROVED AIRPLANEAIRPLANE PERFORMANCEPERFORMANCE New blended winglets on the Boeing Business Jet and the 737-800 commercial airplane offer operational benefits to customers. Besides giving the airplanes a distinctive appear- ance, the winglets create more efficient flight characteristics in cruise and during takeoff and climbout, which translate into additional range with the same fuel and payload. ROBERT FAYE ROBERT LAPRETE MICHAEL WINTER TECHNICAL DIRECTOR ASSOCIATE TECHNICAL FELLOW PRINCIPAL ENGINEER BOEING BUSINESS JETS AERODYNAMICS TECHNOLOGY STATIC AEROELASTIC LOADS BOEING COMMERCIAL AIRPLANES BOEING COMMERCIAL AIRPLANES BOEING COMMERCIAL AIRPLANES TECHNOLOGY/PRODUCT DEVELOPMENT AERO 16 vertical height of the lifting system (i.e., increasing the length of the TE that sheds the vortices). The winglets increase the spread of the vortices along the TE, creating more lift at the wingtips (figs. 2 and 3). The result is a reduction in induced drag (fig. 4). The maximum benefit of the induced drag reduction depends on the spanwise lift distribution on the wing. Theoretically, for a planar wing, induced drag is opti- mized with an elliptical lift distribution that minimizes the change in vorticity along the span. For the same amount of structural material, nonplanar wingtip 737-800 TECHNICAL CHARACTERISTICS devices can achieve a similar induced drag benefit as a planar span increase; however, new Boeing airplane designs Passengers focus on minimizing induced drag with 3-class configuration Not applicable The 737-800 commercial airplane wingspan influenced by additional 2-class configuration 162 is one of four 737s introduced BBJ TECHNICAL CHARACTERISTICS The Boeing Business Jet design benefits. 1-class configuration 189 in the late 1990s for short- to (BBJ) was launched in 1996 On derivative airplanes, performance Cargo 1,555 ft3 (44 m3) medium-range commercial air- Passengers Not applicable as a joint venture between can be improved by using wingtip Boeing and General Electric. -
Poly-Fiber Aircraft Coatings
POLY-FIBER AIRCRAFT COATINGS AIRCRAFT SPRUCE - WORLD’S LARGEST DISTRIBUTOR OF POLY-FIBER PRODUCTS This FAA approved process utilizing Poly-Fiber Dacron polyester and the unique “Poly” line of finishes assures a beautiful, durable, weather-resistant cover job every time. Documented time tested results by the pro fes sion als. The Poly-Fiber Covering Process was CM issued Supplemental Type Cer tifi cate No. SA-1008-WE in 1965 and this number will apply to all aircraft. Note: Formerly known as Stits covering process. Only Poly-Fiber materials may be used through the topcoat paint to comply with STC requirements. Poly-Fiber finishes are required for approval. Poly-Fiber is approved for use on most certified aircraft. To be sure, check the Master Eligibility List in the latest revision of Poly-Fiber Procedure Manual No. 1. WP POLY-FIBER FABRIC UNCERTIFIED LIGHT THE POLY-FIBER 1.87 oz/sq. yard. Lightweight fabric recommended for covering ultralight aircraft. This fabric will be unstamped. PRACTICE KIT It is not approved for certified aircraft except on plywood If you’re thinking of building a fab- surface. 72” Width .... P/N 09-02001 .....$9.65 /Lineal Yd. ric-covered airplane but are won- ME MEDIUM WEIGHT dering what the covering process 2.79 oz/sq. yard. Standard fabric recommended for nor- is like, this is the perfect answer. mal service on all types of aircraft regardless of speed, You get a practice frame, fabric, wing loading or horsepower. tapes, needles, rib lacing cord, P/N 09-01600 ...$13.50 /Lin eal Yd. thermometer, instructions, and all HA HEAVY DUTY the coatings you need to work through the Poly-Spray stage. -
Eaa 430 Flyer
Serving the Port Angeles & Sequim Area EAA 430 FLYER February 2019 Dedicated to having fun with airplanes and promoting General Aviation CHAPTER CHATTER “That's not my job!” This is a story about four individuals named: Everybody, Somebody, Anybody and Nobody. There was an important job to be done and Everybody was sure that Somebody would do it. Anybody could have done it, but Nobody did it. Somebody got angry about that because it was Everybody’s job. Everybody thought Anybody could do it, but Nobody realized that Everybody would not do it. It ended up that Everybody blamed Somebody when Nobody did what Anybody could have done. In our chapter, we are blessed with volunteers who step up. As we continue to grow, we need to expand the numbers of volunteers who pitch in and in come alongside those now serving. I would like to see a mentorship program begin to “train up” the next set of leaders. Doing this will magnify the efforts of the volunteers and spread out the task. This would definitely be a WIN WIN for the chapter. Our March meeting will be in our new home at Sequim Valley Airport. Bud Davies’ hangar #15 will be the location for the near future. Meeting dates and times have not changed … still the last Saturday of the month at 1000. A schedule for the moving day will be determined and a special email announcement will be sent to the membership. Many hands make a large task much smaller. Join us. Several members of the Board of Directors will be attending the EAA BOOT CAMP (leadership training – open to all EAA members) in Puyallup WA on Friday the 22nd. -
Fly-By-Wire: Getting Started on the Right Foot and Staying There…
Fly-by-Wire: Getting started on the right foot and staying there… Imagine yourself getting into the cockpit of an aircraft, finishing your preflight checks, and taxiing out to the runway ready for takeoff. You begin the takeoff roll and start to rotate. As you lift off, you discover your side stick controller is not responding correctly to your commands. Panic sets in, and you feel that you’ve lost total control of the aircraft. Thanks to quick action from your second in command, he takes over and stabilizes the aircraft so that you both can plan to return to the airport under reversionary mode. This situation could have been a catastrophe. This happened in August of 2001. A Lufthansa Airbus A320 came within less than two feet and a few seconds of crashing during takeoff on a planned flight from Frankfurt to Paris. Preliminary reports indicated that maintenance was performed on the captain’s sidestick controller immediately before the incident. This had inadvertently created a situation in which control inputs were reversed. The case reveals that at least two "filters," or safety defenses, were breached, leading to a near-crash shortly after rotation at Frankfurt’s Runway 18. Quick action by the first officer prevented a catastrophe. Lufthansa Technik personnel found a damaged pin on one segment of the four connector segments (with 140 pins on each) at the "rack side," as it were, of the avionics mount. This incident prompted an article to be published in the 2003 November-December issue of the Flight Safety Mechanics Bulletin. The report detailed all that transpired during the maintenance and subsequent release of the aircraft. -
Overview of the Aviation Maintenance Profession
Subject: OVERVIEW OF THE AVIATION Date: 11/09/01 AC No: 65-30A MAINTENANCE PROFESSION Initiated By: AFS-305 Change: 1. PURPOSE. This advisory circular (AC) was prepared by the Federal Aviation Administration (FAA) Flight Standards Service to provide information to prospective airframe and powerplant mechanics and other persons interested in the certification of mechanics. It contains information about the certificate requirements, application procedures, and the mechanic written, oral, and practical tests. 2. CANCELLATION. AC 65-30, Overview of the Aviation Maintenance Profession, dated June 27, 2000, and AC 65-11B, Airframe and Power Plant Mechanics Certification Information, revised in 1987, are canceled. 3. RELATED 14 CFR REFERENCES. Title 14 of the Code of Federal Regulations (14 CFR). a. Part 65, Certification: Airmen other than Flight Crewmembers. b. Part 145, Repair Stations. c. Part 147, Aviation Maintenance Technician Schools. d. Part 187, Fees. 4. RELATED READING MATERIAL. a. To obtain a directory of names and school locations that are FAA certified under the provision of 14 CFR part 147, write to: U.S. Department of Transportation; Subsequent Distribution Office; Ardmore East Business Center; 3341 Q. 75th Ave.; Landover, MD 20785. Request AC 147-2EE, Directory of FAA Certificated Aviation Maintenance Technician Schools. This AC is a free publication. b. For educational assistance, contact the Department of Education, Office of Student Financial Assistance, 400 Maryland Ave, S.W., Washington D.C. 20202. AC 65-30A 11/09/01 c. A comprehensive list of all airlines, repair stations, manufacturers, and fixed base operators (FBO) can be found in the World Aviation Directory at the reference section of your local library. -
Risk Management in Fly-By-Wire Systems
NASA Technical Memorandum 104757 Risk Management in Fly-by-Wire Systems Karyn T. Knoll March 1993 NASA r (NASA-TM-104757) RISK MANAGEMENT N93-22703 IN FLY-BY-WIRE SYSTEMS (NASA) 23 p Unclas G3/17 0156304 NASA Technical Memorandum 104757 Risk Management in Fly-by-Wire Systems KarynT. Knoll Lyndon B. Johnson Space Center Houston, Texas March 1993 National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, Texas CONTENTS Section Page Abstract 1 Introduction . 1 Description of Fly-by-Wire Systems 1 Risks Inherent in Fly-by-Wire Systems 2 Risk Management in the Fly-by-Wire Industry 5 Configuration Control '. 5 Verification and Validation 6 Tools 7 Backup Flight Control Systems 9 Risk Management and the Space Shuttle Program 12 References 17 TABLE Table Page 1 Right Control System Summary 15 PRECEDING PAGE BLANK NOT FILMED Abstract A general description of various types of fly-by-wire systems is provided. The risks inherent in digital flight control systems, like the Space Shuttle, are identified. The results of a literature survey examining risk management methods in use throughout the aerospace industry are presented. The applicability of these methods to the Space Shuttle program is discussed. Introduction Since the development of the Space Shuttle, many other aerospace vehicles have incorporated fly-by-wire technologies in their flight control systems in an effort to improve performance, efficiency, and reliability. Because the flight control system is a critical component of any aerospace vehicle, it is especially important that the risks inherent in using fly-by-wire technologies are thoroughly understood and carefully managed. -
Airframe & Aircraft Components By
Airframe & Aircraft Components (According to the Syllabus Prescribed by Director General of Civil Aviation, Govt. of India) FIRST EDITION AIRFRAME & AIRCRAFT COMPONENTS Prepared by L.N.V.M. Society Group of Institutes * School of Aeronautics ( Approved by Director General of Civil Aviation, Govt. of India) * School of Engineering & Technology ( Approved by Director General of Civil Aviation, Govt. of India) Compiled by Sheo Singh Published By L.N.V.M. Society Group of Institutes H-974, Palam Extn., Part-1, Sec-7, Dwarka, New Delhi-77 Published By L.N.V.M. Society Group of Institutes, Palam Extn., Part-1, Sec.-7, Dwarka, New Delhi - 77 First Edition 2007 All rights reserved; no part of this publication may be reproduced, stored in a retrieval system or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, without the prior written permission of the publishers. Type Setting Sushma Cover Designed by Abdul Aziz Printed at Graphic Syndicate, Naraina, New Delhi. Dedicated To Shri Laxmi Narain Verma [ Who Lived An Honest Life ] Preface This book is intended as an introductory text on “Airframe and Aircraft Components” which is an essential part of General Engineering and Maintenance Practices of DGCA license examination, BAMEL, Paper-II. It is intended that this book will provide basic information on principle, fundamentals and technical procedures in the subject matter areas relating to the “Airframe and Aircraft Components”. The written text is supplemented with large number of suitable diagrams for reinforcing the key aspects. I acknowledge with thanks the contribution of the faculty and staff of L.N.V.M.