| Name | Support | Language | Availability | Edition date | Price | ||
|---|---|---|---|---|---|---|---|
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PDF |
English |
Active |
3/19/2020 |
€101.00 |
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Details
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.
Additional Info
| Author | Society of Automotive Engineers International (SAE) |
|---|---|
| Committee | AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee |
| Published by | SAE |
| Document type | Standard |
| ICS | 49.050 : Aerospace engines and propulsion systems
|
| Number of pages | 16 |
| Replace | SAE AIR 1616A:2012-01-03 |
| Document history | SAE AIR 1616A:2012-01-03,SAE AIR 1616:1983-04-04 |
| Keyword | SAE 1616,SAE AIR1616B,SAE AIR1616B,SAE AIR 1616 |
