Bell 505 Specifications
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United Nations Peacekeeping Missions Military Aviation Unit Manual Second Edition April 2021
UN Military Aviation Unit Manual United Nations Peacekeeping Missions Military Aviation Unit Manual Second Edition April 2021 Second Edition 2019 DEPARTMENT OF PEACE OPERATIONS DEPARTMENT OF OPERATIONAL SUPPORT UN Military Aviation Unit Manual Produced by: Office of Military Affairs, Department of Peace Operations UN Secretariat One UN Plaza, New York, NY 10017 Tel. 917-367-2487 Approved by: Jean-Pierre Lacroix, Under-Secretary-General for Peace Operations Department of Peace Operations (DPO). Atul Khare Under-Secretary-General for Operational Support Department of Operational Support (DOS) April 2021. Contact: PDT/OMA/DPO Review date: 30/ 04 / 2026 Reference number: 2021.04 Printed at the UN, New York © UN 2021. This publication enjoys copyright under Protocol 2 of the Universal Copyright Convention. Nevertheless, governmental authorities or Member States may freely photocopy any part of this publication for exclusive use within their training institutes. However, no portion of this publication may be reproduced for sale or mass publication without the express consent, in writing, of the Office of Military Affairs, UN Department of Peace Operations. ii UN Military Aviation Unit Manual Foreword We are delighted to introduce the United Nations Peacekeeping Missions Military Aviation Unit Manual, an essential guide for commanders and staff deployed in peacekeeping operations, and an important reference for Member States and the staff at United Nations Headquarters. For several decades, United Nations peacekeeping has evolved significantly in its complexity. The spectrum of multi-dimensional UN peacekeeping operations includes challenging tasks such as restoring state authority, protecting civilians and disarming, demobilizing and reintegrating ex-combatants. In today’s context, peacekeeping missions are deploying into environments where they can expect to confront asymmetric threats and contend with armed groups over large swaths of territory. -
The Luftwaffe Wasn't Alone
PIONEER JETS OF WORLD WAR II THE LUFTWAFFE WASN’T ALONE BY BARRETT TILLMAN he history of technology is replete with Heinkel, which absorbed some Junkers engineers. Each fac tory a concept called “multiple independent opted for axial compressors. Ohain and Whittle, however, discovery.” Examples are the incandes- independently pursued centrifugal designs, and both encoun- cent lightbulb by the American inventor tered problems, even though both were ultimately successful. Thomas Edison and the British inventor Ohain's design powered the Heinkel He 178, the world's first Joseph Swan in 1879, and the computer by jet airplane, flown in August 1939. Whittle, less successful in Briton Alan Turing and Polish-American finding industrial support, did not fly his own engine until Emil Post in 1936. May 1941, when it powered Britain's first jet airplane: the TDuring the 1930s, on opposite sides of the English Chan- Gloster E.28/39. Even so, he could not manufacture his sub- nel, two gifted aviation designers worked toward the same sequent designs, which the Air Ministry handed off to Rover, goal. Royal Air Force (RAF) Pilot Officer Frank Whittle, a a car company, and subsequently to another auto and piston 23-year-old prodigy, envisioned a gas-turbine engine that aero-engine manufacturer: Rolls-Royce. might surpass the most powerful piston designs, and patented Ohain’s work detoured in 1942 with a dead-end diagonal his idea in 1930. centrifugal compressor. As Dr. Hallion notes, however, “Whit- Slightly later, after flying gliders and tle’s designs greatly influenced American savoring their smooth, vibration-free “Axial-flow engines turbojet development—a General Electric– flight, German physicist Hans von Ohain— were more difficult built derivative of a Whittle design powered who had earned a doctorate in 1935— to perfect but America's first jet airplane, the Bell XP-59A became intrigued with a propeller-less gas- produced more Airacomet, in October 1942. -
FAA Order 8130.2H, February 4, 2015
U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADM INISTRATION ORDER 8130.2H 02/04/2015 National Policy SUBJ: Airworthiness Certification of Products and Articles This order establishes procedures for accomplishing original and recurrent airworthiness certification ofaircraft and related products and articles. The procedures contained in this order apply to Federal Aviation Administration (FAA) manufacturing aviation safety inspectors (ASI), to FAA airworthiness AS Is, and to private persons or organizations delegated authority to issue airworthiness certificates and related approvals. Suggestions for improvement of this order may be submitted using the FAA Office of Aviation Safety (AVS) directive feedback system at http://avsdfs.avs.faa.gov/default.aspx, or FAA Form 1320-19, Directive Feedback Information, found in appendix I to this order. D G!JD Cf1 · ~ David Hempe Manager, Design, Manufacturing, & Airworthiness Division Aircraft Certification Service Distribution: Electronic Initiated By: AIR-1 00 02/04/2015 8130.2H Table of Contents Paragraph Page Chapter 1. Introduction 100. Purpose of This Order .............................................................................. 1-1 101. Audience .................................................................................................. 1-1 102. Where Can I Find This Order .................................................................. 1-1 103. Explanation of Policy Changes ................................................................ 1-1 104. Cancellation ............................................................................................ -
2015 Annual Report 2015 Annual
2015 ANNUAL 2015 ANNUAL REPORT 2015 ANNUAL REPORT Textron’s Diverse Product Portfolio Textron is known around the world for its powerful brands of aircraft, defense and industrial products that provide customers with groundbreaking technologies, innovative solutions and first-class service. TEXTRON AVIATION BELL HELICOPTER INDUSTRIAL TEXTRON SYSTEMS Citation® Longitude® Bell Boeing V-22 Osprey Sherman + ReillyTM P2000X Puller Shadow® M2 Citation® M2® Bell 429WLG E-Z-GO Freedom® RXV Lycoming Race Engines Beechcraft® King Air® 350i Bell 525 RelentlessTM Greenlee® DataScout® 10Gx TRU Level D Full Flight Simulator Cessna® TTx® Bell 407GXP Kautex NGFS® Fuel Tank Ship to Shore Connector (SSC) Beechcraft® T-6 Military Trainer Bell 412EPI Dixie Chopper® Stryker Stand-on FuryTM Precision Guided Weapon Cessna® Grand Caravan® EX Bell 505 Jet Ranger XTM TUGTM MA Tow Tractor COMMANDOTM Elite Textron’s Global Network of Businesses TEXTRON AVIATION BELL HELICOPTER INDUSTRIAL TEXTRON SYSTEMS FINANCE Textron Aviation is home Bell Helicopter is one Our Industrial segment Textron Systems’ Our Finance segment, to the iconic Beechcraft, of the leading suppliers offers three main businesses provide operated by Textron Cessna and Hawker of helicopters and product lines: fuel innovative solutions to Financial Corporation brands, and continues related spare parts and systems and functional the defense, aerospace (TFC), is a commercial to lead general aviation services in the world. components produced and general aviation finance business that through two principal Bell is the pioneer of by Kautex; specialized markets. Product lines provides financing lines of business: aircraft the revolutionary tiltrotor vehicles and equipment include unmanned solutions for purchasers of sales and aftermarket. -
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. -
Bell 429 Product Specifications
BELL 429 SPECIFICATIONS BELL 429 SPECIFICATIONS Publisher’s Notice The information herein is general in nature and may vary with conditions. Individuals using this information must exercise their independent judgment in evaluating product selection and determining product appropriateness for their particular purpose and requirements. For performance data and operating limitations for any specific mission, reference must be made to the approved flight manual. Bell Helicopter Textron Inc. makes no representations or warranties, either expressed or implied, including without limitation any warranties of merchantability or fitness for a particular purpose with respect to the information set forth herein or the product(s) and service(s) to which the information refers. Accordingly, Bell Helicopter Textron Inc. will not be responsible for damages (of any kind or nature, including incidental, direct, indirect, or consequential damages) resulting from the use of or reliance on this information. Bell Helicopter Textron Inc. reserves the right to change product designs and specifications without notice. © 2019 Bell Helicopter Textron Inc. All registered trademarks are the property of their respective owners. FEBRUARY 2019 © 2019 Bell Helicopter Textron Inc. Specifications subject to change without notice. i BELL 429 SPECIFICATIONS Table of Contents Bell 429 ..................................................................................................................................1 Bell 429 Specification Summary (U.S. Units) ........................................................................4 -
Aerospace Facts and Figures 1983/84
Aerospace Facts and Figures 1983/84 AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA, INC. 1725 DeSales Street, N.W., Washington, D.C. 20036 Published by Aviation Week & Space Technology A MCGRAW-HILL PUBLICATION 1221 Avenue of the Americas New York, N.Y. 10020 (212) 997-3289 $9.95 Per Copy Copyright, July 1983 by Aerospace Industries Association o' \merica, Inc. · Library of Congress Catalog No. 46-25007 2 Compiled by Economic Data Service Aerospace Research Center Aerospace Industries Association of America, Inc. 1725 DeSales Street, N.W., Washington, D.C. 20036 (202) 429-4600 Director Research Center Virginia C. Lopez Manager Economic Data Service Janet Martinusen Editorial Consultant James J. Haggerty 3 ,- Acknowledgments Air Transport Association of America Battelle Memorial Institute Civil Aeronautics Board Council of Economic Advisers Export-Import Bank of the United States Exxon International Company Federal Trade Commission General Aviation Manufacturers Association International Civil Aviation Organization McGraw-Hill Publications Company National Aer~mautics and Space Administration National Science Foundation Office of Management and Budget U.S. Departments of Commerce (Bureau of the Census, Bureau of Economic Analysis, Bureau of Industrial Economics) Defense (Comptroller; Directorate for Information, Operations and Reports; Army, Navy, Air Force) Labor (Bureau of Labor Statistics) Transportation (Federal Aviation Administration The cover and chapter art throughout this edition of Aerospace Facts and Figures feature computer-inspired graphics-hot an original theme in the contemporary business environment, but one particularly relevant to the aerospace industry, which spawned the large-scale development and application of computers, and conti.nues to incorpora~e computer advances in all aspects of its design and manufacture of aircraft, mis siles, and space products. -
ICE PROTECTION Incomplete
ICE PROTECTION GENERAL The Ice and Rain Protection Systems allow the aircraft to operate in icing conditions or heavy rain. Aircraft Ice Protection is provided by heating in critical areas using either: Hot Air from the Pneumatic System o Wing Leading Edges o Stabilizer Leading Edges o Engine Air Inlets Electrical power o Windshields o Probe Heat . Pitot Tubes . Pitot Static Tube . AOA Sensors . TAT Probes o Static Ports . ADC . Pressurization o Service Nipples . Lavatory Water Drain . Potable Water Rain removal from the Windshields is provided by two fully independent Wiper Systems. LEADING EDGE THERMAL ANTI ICE SYSTEM Ice protection for the wing and horizontal stabilizer leading edges and the engine air inlet lips is ensured by heating these surfaces. Hot air supplied by the Pneumatic System is ducted through perforated tubes, called Piccolo tubes. Each Piccolo tube is routed along the surface, so that hot air jets flowing through the perforations heat the surface. Dedicated slots are provided for exhausting the hot air after the surface has been heated. Each subsystem has a pressure regulating/shutoff valve (PRSOV) type of Anti-icing valve. An airflow restrictor limits the airflow rate supplied by the Pneumatic System. The systems are regulated for proper pressure and airflow rate. Differential pressure switches and low pressure switches monitor for leakage and low pressures. Each Wing's Anti Ice System is supplied by its respective side of the Pneumatic System. The Stabilizer Anti Ice System is supplied by the LEFT side of the Pneumatic System. The APU cannot provide sufficient hot air for Pneumatic Anti Ice functions. -
Chapter 76 Engine Controls
ENGINE CONTROLS XL-2 AIRPLANE CHAPTER 76 ENGINE CONTROLS P/N 135A-970-100 Chapter 76 REVISION ~ Page 1 of 18 ENGINE CONTROLS XL-2 AIRPLANE Copyright © 2009 All rights reserved. The information contained herein is proprietary to Liberty Aerospace, Incorporated. It is prohibited to reproduce or transmit in any form or by any means, electronic or mechanical, including photocopying, recording, or use of any information storage and retrieval system, any portion of this document without express written permission of Liberty Aerospace Incorporated. Chapter 76 P/N 135A-970-100 Page 2 of 18 REVISION ~ ENGINE CONTROLS XL-2 AIRPLANE Table of Contents SECTION 76-00 GENERAL 5 SECTION 00-01 FADEC SYSTEM DESCRIPTION AND FUNCTIONAL OVERVIEW 6 SECTION 00-02 HEALTH STATUS ANNUNCIATOR AND POWER TRANSFER CHECK PROCEDURES 7 FADEC POWER TRANSFER CHECK 8 SECTION 76-10 POWER CONTROL 11 SECTION 10-01 POWER (THROTTLE) CABLE REMOVAL AND REPLACEMENT 12 THROTTLE CABLE REMOVAL 13 THROTTLE CABLE INSTALLATION 14 THROTTLE CABLE RIGGING PROCEDURE 15 SECTION 76-20 EMERGENCY SHUTDOWN 17 P/N 135A-970-100 Chapter 76 REVISION ~ Page 3 of 18 ENGINE CONTROLS XL-2 AIRPLANE PAGE LEFT INTENTIONALLY BLANK. Chapter 76 P/N 135A-970-100 Page 4 of 18 REVISION ~ ENGINE CONTROLS XL-2 AIRPLANE Section 76-00 General This chapter provides a descriptive overview of the control systems for the IOF- 240-B engine installed on the airplane. Detailed information for routine line maintenance for each engine subsection or system is provided in the appropriate chapter. More detailed information for repairs and maintenance on systems and components specific to the IOF-240B engine FADEC system are provided in the current release of the Teledyne Continental Motors Maintenance Manual for IOF- 240-B series engines, TCM p/n: M-22. -
AED Fleet Contact List
AED Fleet Contact List September 2021 Make Model Primary Office Operations - Primary Operations - Secondary Avionics - Primary Avionics - Secondary Maintenance - Primary Maintenance - Secondary Air Tractor All Models MKC Persky, David (FAA) Hawkins, Kenneth (FAA) Marsh, Kenneth (FAA) Rockhill, Thane D (FAA) BadHorse, Jim (FAA) Airbus A300/310 SEA Hutton, Rick (FAA) Dunn, Stephen H (FAA) Gandy, Scott A (FAA) Watkins, Dale M (FAA) Patzke, Roy (FAA) Taylor, Joe (FAA) Airbus A318-321 CEO/NEO SEA Culet, James (FAA) Elovich, John D (FAA) Watkins, Dale M (FAA) Gandy, Scott A (FAA) Hunter, Milton C (FAA) Dodd, Mike B (FAA) Airbus A330/340 SEA Culet, James (FAA) Robinson, David L (FAA) Flores, John A (FAA) Watkins, Dale M (FAA) DiMarco, Joe (FAA) Johnson, Rocky (FAA) Airbus A350 All Series SEA Robinson, David L (FAA) Culet, James (FAA) Watkins, Dale M (FAA) Flores, John A (FAA) Dodd, Mike B (FAA) Johnson, Rocky (FAA) Airbus A380 All Series SEA Robinson, David L (FAA) Culet, James (FAA) Flores, John A (FAA) Watkins, Dale M (FAA) Patzke, Roy (FAA) DiMarco, Joe (FAA) Aircraft Industries All Models, L-410 etc. MKC Persky, David (FAA) McKee, Andrew S (FAA) Marsh, Kenneth (FAA) Pruneda, Jesse (FAA) Airships All Models MKC Thorstensen, Donald (FAA) Hawkins, Kenneth (FAA) Marsh, Kenneth (FAA) McVay, Chris (FAA) Alenia C-27J LGB Nash, Michael A (FAA) Lee, Derald R (FAA) Siegman, James E (FAA) Hayes, Lyle (FAA) McManaman, James M (FAA) Alexandria Aircraft/Eagle Aircraft All Models MKC Lott, Andrew D (FAA) Hawkins, Kenneth (FAA) Marsh, Kenneth (FAA) Pruneda, -
Bell Uh-1 Iroquois
BELL UH-1 IROQUOIS UH-1 SERVICE Manufacturer: Bell Helicopter Corp. of Bell Aircraft Corp., Fort Worth, Texas, USA (In 1960, became Bell Helicopter Co., Textron Corp.) (In 1976, became Bell Helicopter Textron, Textron Inc.) Models: Model 204, 205, 208, 210, 211, 212, 214, 412, 450, 533, 577 Designations: H-1 (UH-1); H-40, H-48, HU-1, CH-118 / CH-135 / CH-146 (CAF) Names: Iroquois; Huey (unofficial), Venom & Super Huey (UH-1Y) First official flight: XH-40 22/10/1956 Factory production period: 1955 – 1987 (military) 1963 – present (civil) Primary service period: 1959 – 1980’s Last official flight: - - UH-1 VARIANTS 1956 Model 204 XH-40 3 1956 Model 204 YH-40 6 Total: 00009 1959 Model 204 HU-1A (UH-1A) 182 1960 Model 204 YHU-1B (YUH-1B) 4 1961 Model 204 HU-1B (UH-1B) 1030 1965 Model 204 UH-1C 755 Total: 01971 1961 Model 205 YHU-1D (YUH-1D) 7 1963 Model 205 UH-1D 2010 Total: 02017 1963 Model 204 UH-1E 209 1964 Model 204 UH-1F 120 1967 Model 204 TH-1F 26 Total: 00355 1967 Model 205 UH-1H 5648 1968 Model 205 CUH-1H 10 1971 Model 205 HH-1H 30 Total: 05688 1969 Model 204 HH-1K 27 1969 Model 204 TH-1L 90 1968 Model 204 UH-1L 8 Total: 00125 1969 Model 212 UH-1N 288 1971 Model 212 CUH-1N 50 1974 Model 212 VH-1N 6 Total: 00344 2006 Model 450 UH-1Y 135 Total: 00135 1962 Model 204 Model 204 80 1968 Model 205 Model 205 332 1969 Model 212 Model 212 917 1970 Model 214 Model 214 509 1981 Model 412 Model 412 1026 Total: 02864 Total: 13508 Foreign built – Indonesia: 1986 Model 412 NBell 412 30 Total: 00030 Foreign built – Italy: 1961 Model 204 Model AB.204 -
Aircraft Collection
A, AIR & SPA ID SE CE MU REP SEU INT M AIRCRAFT COLLECTION From the Avenger torpedo bomber, a stalwart from Intrepid’s World War II service, to the A-12, the spy plane from the Cold War, this collection reflects some of the GREATEST ACHIEVEMENTS IN MILITARY AVIATION. Photo: Liam Marshall TABLE OF CONTENTS Bombers / Attack Fighters Multirole Helicopters Reconnaissance / Surveillance Trainers OV-101 Enterprise Concorde Aircraft Restoration Hangar Photo: Liam Marshall BOMBERS/ATTACK The basic mission of the aircraft carrier is to project the U.S. Navy’s military strength far beyond our shores. These warships are primarily deployed to deter aggression and protect American strategic interests. Should deterrence fail, the carrier’s bombers and attack aircraft engage in vital operations to support other forces. The collection includes the 1940-designed Grumman TBM Avenger of World War II. Also on display is the Douglas A-1 Skyraider, a true workhorse of the 1950s and ‘60s, as well as the Douglas A-4 Skyhawk and Grumman A-6 Intruder, stalwarts of the Vietnam War. Photo: Collection of the Intrepid Sea, Air & Space Museum GRUMMAN / EASTERNGRUMMAN AIRCRAFT AVENGER TBM-3E GRUMMAN/EASTERN AIRCRAFT TBM-3E AVENGER TORPEDO BOMBER First flown in 1941 and introduced operationally in June 1942, the Avenger became the U.S. Navy’s standard torpedo bomber throughout World War II, with more than 9,836 constructed. Originally built as the TBF by Grumman Aircraft Engineering Corporation, they were affectionately nicknamed “Turkeys” for their somewhat ungainly appearance. Bomber Torpedo In 1943 Grumman was tasked to build the F6F Hellcat fighter for the Navy.