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 »

Preview Document Add to Cart
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.
We also recommend:
STANDARD

Overview and History of Aircraft Inerting Systems

AIR1903A

View Details

STANDARD

Aircraft Turbine Fuel Contamination History and Endurance Test Requirements

AIR4023C

View Details

STANDARD

Design and Operating Requirements of the Onboard Aircraft Refueling System and Associated Ground Refueling Equipment Interface

AS5751

View Details

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X