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Parts Safety Vehicle drivers Vehicle occupants Analysis methodologies Lightning Identification AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee

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Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems
2020-03-19
CURRENT
AIR1616B
MIL-STD-1290, 14 CFR 27.952, and 14 CFR 29.952 provide crash resistant fuel system design and test criteria that significantly minimize fuel leaks and occurrence of post-crash fire in survivable impacts. This document does not change and does not authorize changes in or deviations from MIL-Standard or regulatory requirements. This document provides guidance for the design, performance, and test criteria for self-sealing breakaway valves.
Standard

Thesaurus for Fuel System Components
2007-12-04
HISTORICAL
AIR1615A
This document provides a summary of names commonly used throughout the industry for aircraft fuel system components. It is a thesaurus intended to aid those not familiar with the lexicon of the industry.
Standard

Thesaurus for Fuel System Components
2020-02-24
CURRENT
AIR1615B
This document provides a summary of names commonly used throughout the industry for aircraft fuel system components. It is a thesaurus intended to aid those not familiar with the lexicon of the industry.
Standard

Optical equipment safety in fuel tanks
2018-11-15
WIP
ARP7977
This project aims to develop a framework of requirements which support safe installation and operation of optical devices within an aircraft fuel tank, specifically: 1: To determine optical power and energy limits which ensure safe operation of optical installations within an aircraft fuel tank over aircraft life and under all phases of flight, taking the limits provided in IEC 60079-28:20015 as a starting point. 2: To demonstrate optical and electrical power and energy equivalences, where possible. 3: To determine requirements for optical installations, including bonding and electrostatic discharge for non-conductive components such as optical fibres. 4: To provide guidelines for analysis of the hazards presented by the typical internal components of optical devices, such as failure modes of photo diodes and cells.
Standard

Aircraft Flame Arrestor Installation Guidelines and Test Methods
2021-08-26
CURRENT
ARP5776
The scope of this document is to provide pertinent information on demonstrating the performance of Flame Arrestors, also known as Fuel Vent Protectors (FVPs), in preventing the propagation of a deflagration when the arrestors are subjected to aerospace-representative flames produced by the venting of flammable gas through the arrestor. Test procedures for two separate combustion-loading profiles are presented herein: The flame hold test condition, and the flame propagation test condition. For the flame hold test condition, the applicability of two separate critical flows is discussed in which one flow results in the greatest flame arrestor temperature and a second flow results in the greatest temperature of the surrounding structure.
Standard

Aerospace Fuel System Specifications and Standards
2007-12-04
HISTORICAL
AIR1408A
This report lists documents that aid and govern the design of gas turbine powered aircraft and missile fuel systems. The report lists the military and industry specifications and standards and the most notable design handbooks that are commonly used in fuel system design. The specifications and standards section has been divided into two parts, a master list arranged numerically of all industry and military specifications and standards and a component list that provides a functional breakdown and a cross-reference of these documents. It is intended that this report be a supplement to specifications MIL-F-8615, MIL-F-17874, MIL-F-38363 and MIL-F-87154. Revisions and amendments which are correct for the specifications and standards are not listed. The fuel system design handbooks are listed for fuels and for system and component design.
Standard

AEROSPACE FUEL SYSTEM SPECIFICATIONS AND STANDARDS
1976-03-01
HISTORICAL
AIR1408
This report lists military and industry specifications and standards which are commonly used in aerospace gas turbine fuel systems. It is intended as a supplement to specifications MIL-F-3863, MIL-F-17874 and MIL-F-8615. Revisions and amendments which are current for these specifications and standards are not listed.
Standard

Fuel Level Point Sensing
2020-11-30
CURRENT
AIR6325
This report is intended to identify the various existing technologies used for a fuel level sensing system. In addition to sensing technologies, it describes the basic architecture of fuel level sensing systems and their association with fuel gauging system to increase integrity of fuel measurement and management. As the fuel level sensing system is generally based on electrical components within fuel tanks, a specific focus is made on fuel tank explosion safety protection. An overview of the capacitive fuel gauging operation can be found in AIR5691.
Standard

GLOSSARY OF TERMS - AIRCRAFT GROUND REFUELING
2007-12-04
HISTORICAL
AIR4783
This SAE Aerospace Information Report (AIR) presents a glossary of terns commonly utilized in the ground delivery of fuel to an aircraft and some terms relating to the aircraft being refueled.
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