AIR1616B: Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems - Information Report

Features

Issuing Committee: AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee

Scope

Content: 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.

Meta Tags

Topics: Fuel systems
Failure modes and effects analysis (FMEA)
Jet fuel
Rotary-wing aircraft
Valves

Details

DOI: https://doi.org/10.4271/AIR1616B

Pages: 16

Citation: SAE International Information Report, Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems, SAE Standard AIR1616B, Revised March 2020, Stabilized January 2012, Issued April 1983, https://doi.org/10.4271/AIR1616B.

Additional Details

Publisher: SAE International

Published: Mar 19, 2020

Product Code: AIR1616B

Content Type: Information Report

Status: Revised

Language: English

Historical