Browse Standards AIR1616B
Current REVISED 2020-03-19

Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems(STABILIZED Jan 2012) 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.
AIR1616B
2020-03-19
Latest
Revised
AIR1616A
2012-01-03
Historical
Stabilized
AIR1616
1983-04-04
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 10% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.

Due to current capacity constraints, printed versions of our publications - including standards, technical papers, EDGE Reports, scholarly journal articles, books, and paint chips - may experience shipping delays of up to four to six weeks. We apologize for any inconvenience.
We also recommend:
TECHNICAL PAPER

Crash-Resistant Fuel Systems for General Aviation Aircraft

790592

View Details

TECHNICAL PAPER

Crash-Resistant Fuel Tanks for Helicopters and General Aviation Aircraft

740358

View Details

MAGAZINE

The S.A.E. Journal of Automotive Engineering 1972-10-01

SAEJ1072

View Details

Get Involved

Want to participate in updating this standard?

X