| Nom | Support | Langue | Disponibilité | Date d'édition | Prix | ||
|---|---|---|---|---|---|---|---|
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PDF |
Anglais |
Active |
19/03/2020 |
101,00 € |
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Détails
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.
Informations supplémentaires
| Auteur | Society of Automotive Engineers International (SAE) |
|---|---|
| Comité | AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee |
| Edité par | SAE |
| Type de document | Norme |
| ICS | 49.050 : Moteurs et systèmes de propulsion aérospatiaux
|
| Nombre de pages | 16 |
| Remplace | SAE AIR 1616A:2012-01-03 |
| Historique | SAE AIR 1616A:2012-01-03,SAE AIR 1616:1983-04-04 |
| Mot-clé | SAE 1616,SAE AIR1616B,SAE AIR1616B,SAE AIR 1616 |
