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SAE AS8584 - BRAKE SYSTEMS, WHEEL, MILITARY AIRCRAFT Organization: SAE
Date: 2013-11-01
Description: 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.
SAE AIR1899 - AEROSPACE MILITARY AIRCRAFT HYDRAULIC SYSTEM CHARACTERISTICS Organization: SAE
Date: 2001-03-01
Description: •Attack Airplanes •Fighter Airplanes •Bombers •Anti-Sub, Fixed Wing Airplanes •Transport Airplanes •Helicopters •Boats 1.1 Purpose: The purpose of this document is to provide hydraulic system information to military vehicle system and component designers in order to assist them in future aircraft fluid power system designs.
NPFC - MIL-STD-805 - TOWING FITTINGS AND PROVISIONS FOR MILITARY AIRCRAFT, DESIGN REQUIREMENTS FOR Organization: NPFC
Date: 1987-09-07
Description: It is intended that this standard shall be applicable to all newly developed military aircraft. As a goal, it is desirable that commercial or modified commercial aircraft be equipped with towing fittings that are compatible with existing DOD inventory ground support equipment towbars.
TSE - TS 2924 - LEAD-ACIDS BATTERY FOR MILITARY AIRCRAFT, VEHICLE AND STATIONARY UNIT Organization: TSE
Date: 1978-04-29
Description: This standard covers the lead-acids battery for military aircraft, vehicle and stationary unit. Bu standard, askeri uçak, araç ve sabit tesislerde kullanılan 6 V 12 V ve 24 V anma gerilimlerine sahip kurşun-asit Akümülatörlerini kapsar.
NPFC - MIL-STD-3023 - HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR MILITARY AIRCRAFT Organization: NPFC
Date: 2011-11-21
Description: 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.
SAE/TP - 2009-01-3112 - MAN MACHINE INTERFACE REQUIREMENT VALIDATION IN MILITARY AIRCRAFT CERTIFICATION Organization: SAE/TP
Date: 2009-11-10
Description: Increasing electronic controls in aircraft flight deck, especially in military aircrafts, demands special attention from crew workload assessment and human error analysis point of view.
SAE AIR1083 - (R) AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT Organization: SAE
Date: 2012-04-01
Description: 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.
SAE AIR1603 - AUXILIARY POWER SYSTEM CONSIDERATIONS FOR ADVANCED MILITARY AIRCRAFT Organization: SAE
Date: 1993-06-17
Description: This document provides a brief description of the auxiliary power equipment that is available with enough description and pertinent comments to enable an engineer to make logical preliminary selection of the appropriate equipment for advanced military aircraft programs. The information has been kept as brief as possible to include the maximum amount of equipment in a relatively short document.
SAE ARP1493 - WHEEL AND HYDRAULICALLY ACTUATED BRAKE DESIGN AND TEST REQUIREMENTS FOR MILITARY AIRCRAFT Organization: SAE
Date: 2013-11-01
Description:   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 are airframe and military personnel who prepare detail design and performance specifications.
AIR FORCE - MIL-T-7935A - TOWING REQUIREMENTS AND PROVISIONS FOR LAND AND CARRIER TYPE MILITARY AIRCRAFT Organization: AIR FORCE
Date: 1956-06-20
Description: This specification covers general requirements and provisions for towing all heavier-than-air military aircraft equipped with wheel-type alighting gear. Provisions apply only to those fittings which are an integral part of the aircraft, and not to auxiliary towing equipment.
NAVY - OPNAV 3770.4 - (OP-513H) USE OF AIRSPACE BY U.S. MILITARY AIRCRAFT AND FIRING OVER THE HIGH SEAS Organization: NAVY
Date: 1981-03-23
Description: DEPARTMENT OF THE NAVY OFFICE OF THE CHIEF OF NAVAL OPERATIONS WASHINGTON, D.C. 20350 IN REPLY REFER TO OPNAVINST 3770.4A Op-513H MAR 23 1981 OPNAV INSTRUCTION 3770.4A From: Chief of Naval Operations Subj: Use of Airspace by U. S. Military Aircraft and Firing Over the High Seas Encl: (1) DOD Directive 4540.1 of 13 Jan 1981
DODD 4540.01 - USE OF INTERNATIONAL AIRSPACE BY U.S. MILITARY AIRCRAFT AND FOR MISSILE AND PROJECTILE FIRINGS Organization: DODD
Date: 2015-06-02
Description: Reissues DoD Instruction (DoDI) 4540.01 (Reference (c)) to establish policy and assign responsibilities governing U.S. military aircraft operations and missile and projectile firing activities in international airspace.
SAE AS94900 - AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR Organization: SAE
Date: 2007-07-01
Description: This specification establishes general performance, design, test, development and quality assurance requirements for the Flight Control Systems of military piloted aircraft. Flight Control Systems (FCS) include all components used to transmit flight control commands from the pilot or other sources to appropriate force and moment producers.
SAE ARP5796 - FLIGHT CRITICAL CONTROL VALVES, MILITARY AIRCRAFT Organization: SAE
Date: 2013-07-01
Description: 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 could cause a catastrophic failure resulting in death, permanent total disability, and/or financial loss exceeding a defined contractual limit.
DIN - LN 29766-2 - IDENTIFICATION PLATES FOR AIRCRAFT; MILITARY AIRCRAFTS Organization: DIN
Date: 1970-06-01
NPFC - MIL-STD-1333 - AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT Organization: NPFC
NPFC - MIL-STD-850 - AIRCREW STATION VISION REQUIREMENTS FOR MILITARY AIRCRAFT Organization: NPFC
EURO - PSC/87/18535 - LIFE CYCLE COST PERSPECTIVES - MILITARY AIRCRAFT APPLICATIONS Organization: EURO
Date: 1987-01-01
NAVY - OPNAV 3722.5E - IDENTIFICATION AND SECURITY CONTROL OF MILITARY AIRCRAFT Organization: NAVY
Date: 1970-04-17
NPFC - MIL-C-38747 - COVERING, FLOOR, MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR Organization: NPFC

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