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AIRCRAFT FIRE PROTECTION FOR HELICOPTER GAS TURBINE POWERPLANT AND RELATED SYSTEMS INSTALLATIONS
- Aerospace Standard
Published May 01, 1989 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document is reissued for application to helicopters. It is primarily intended to apply to the engine or engines, but it shall also apply to fire protection of lines, tanks, combustion heaters, and auxiliary powerplants (APU). Post-crash fire protection is also discussed.
|Aerospace Standard||ENGINE EXHAUST SYSTEM DESIGN CONSIDERATIONS FOR ROTORCRAFT|
|Aerospace Standard||AIRCRAFT FIRE PROTECTION FOR RECIPROCATING AND GAS TURBINE ENGINE INSTALLATIONS|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|Unnamed Dataset 4|
|Unnamed Dataset 5|
|Unnamed Dataset 6|
S-12 Powered Lift Propulsion Committee
|FAR29||This document is not part of the subscrption.|
|MIL-HDBK-221(WP||This document is not part of the subscrption.|
|MIL-HDBK-221(WP)||This document is not part of the subscrption.|
|U. S. Navy Spec. SD-24K||This document is not part of the subscrption.|
|U.S.NavySpec.SD||This document is not part of the subscrption.|
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