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TRA AIRCRAFT TIRES - ENGINEERING DESIGN INFORMATION FOR AIRCRAFT TIRES
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TRA AIRCRAFT YEAR BOOK - AIRCRAFT YEAR BOOK
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SAE AIR6245 - Perspectives on Integrating Structural Health Monitoring Systems into Fixed-Wing Military Aircraft
November 1, 2018 - SAE

This SAE Aerospace Information Report (AIR) is prepared for stakeholders seeking information about the evolution, integration, and approval of SHM technologies for military aircraft systems. The report provides this information in the form of (a) two military organizations'...

SAE AS8584 - Brake Systems, Wheel, Military Aircraft
November 1, 2013 - SAE

This SAE Aerospace Standard (AS) defines the requirements for brake systems used on military aircraft equipped with wheel-type landing gears. Product Classification Brake systems shall be either mechanical, hydraulic, pneumatic, electric or a combination of each. Braking force control...

SAE AS94900 - (R) Vehicle Management Systems - Flight Control Function, Design, Installation and Test of Piloted Military Aircraft, General Specification For
August 1, 2018 - SAE

This SAE Aerospace Standard (AS) provides the general performance, design, installation, test, development, and quality assurance requirements for the flight control related functions of the Vehicle Management Systems (VMS) of military piloted aircraft. It also provides specification...

ANSI/ASA S12.76 - AMERICAN NATIONAL STANDARD Methods for Measurement of Supersonic Jet Noise from Uninstalled Military Aircraft Engines
March 27, 2017 - ASA

This standard describes procedures to measure jet noise from uninstalled military aircraft engines with supersonic exhaust flows. The methods pertain to propulsion systems mounted on outdoor test stands with appropriate inlets and representative nozzles. Detailed measurement...

SAE ARP5796 - Flight Critical Control Valves, Military Aircraft
July 1, 2013 - SAE

This SAE Aerospace Recommended Practice (ARP) provides guidance in the design, development, qualification test, process control and production acceptance test for flight critical control valve (FCCV) design used in military flight control servoactuators where loss of single valve control...

SAE ARP1493 - Wheel and Hydraulically Actuated Brake Design and Test Requirements for Military Aircraft
November 1, 2013 - SAE

This document covers military aircraft wheel and hydraulically actuated brake equipment. Purpose This document provides recommended practices for designing and testing wheels and hydraulically actuated brakes for use on new designs of military aircraft. Intended users...

MIL-STD-3023 - High-Altitude Electromagnetic Pulse (HEMP) Protection for Military Aircraft
November 21, 2011 - NPFC

This Standard establishes design margin, performance metrics, and test protocols for high-altitude electromagnetic pulse (HEMP) protection of military aircraft with nuclear EMP survivability at three hardness levels: level I, level II and level III. This Standard may also be used for...

SAE AIR1083 - (R) Airborne Hydraulic and Control System Survivability for Military Aircraft
April 1, 2012 - SAE

This SAE Aerospace Information Report (AIR) provides the hydraulic and flight-control system designer with the various design options and techniques that are currently available to enhance the survivability of military aircraft. The AIR addresses the following major topics: a. Design...

SAE AS5440 - (R) Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For
January 1, 2011 - SAE

This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems. Classification Aircraft hydraulic systems shall be of the following types and classes, as specified: Types: Type I Maximum fluid operating temperature +160°F (+71°C). Type...

A-A-58026 - TRACTOR, AIRCRAFT TOWING, U-30
June 6, 2018 - NPFC

This Commercial Item Description (CID) covers the requirements for the U-30 aircraft-towing tractor, hereafter referred to as tow tractor. The tow tractor is capable of towing military aircraft weighing up to 850,000 pounds and commercial aircraft weighing up to...

SAE ARP4418 - (R) Procedure for Sampling and Measurement of Aircraft Propulsion Engine and APU Generated Contaminants in Bleed Air
November 1, 2018 - SAE

This ARP outlines recommended practices to quantify the concentrations of a subset of bleed air contaminant marker compounds on an aircraft propulsion engine or APU prior to delivery and installation on civil and military aircraft. Testing is specified during steady state...

SAE ARP5908 - (R) Landing Gear Servicing
July 1, 2018 - SAE

The present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber (also know as dual stage and two stage) shock This document should be considered as landing gear industry recommended practice...

SAE AIR1899 - Aerospace Military Aircraft Hydraulic System Characteristics
March 1, 2001 - SAE

1. SCOPE: This SAE Aerospace Information Report (AIR) has been compiled to provide information on hydraulic systems fitted to the following categories of military vehicles. •Attack Airplanes •Fighter Airplanes •Bombers •Anti-Sub, Fixed Wing Airplanes •Transport Airplanes •Helicopters •Boats...

DEF STAN 00-970: PART 11 - Design and Airworthiness Requirements for Service Aircraft Part 11: Engines
May 14, 2018 - MODUK

INTRODUCTION This Part of the Defence Standard has been issued to provide requirements and guidance for the certification of UK military aircraft engines. This standard has been developed in full consideration of European civil certification requirements to ensure that the design of...

SAE ARP4553 - (R) Self-Displacing Hydraulic Accumulator
September 1, 2018 - SAE

SCOPE This SAE Aerospace Recommended Practice (ARP) provides recommendations for design and test requirements for selfdisplacing hydraulic accumulators. Purpose The recommended requirements contained in this ARP are compiled for inclusion, as applicable, in a Procurement Specification for this type...

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