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AIRCRAFT FIRE PROTECTION FOR HELICOPTER GAS TURBINE POWERPLANT AND RELATED SYSTEMS INSTALLATIONS
- Aerospace Standard
- AIR1262
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Recommended Content
| Aerospace Standard | ENGINE EXHAUST SYSTEM DESIGN CONSIDERATIONS FOR ROTORCRAFT |
| Aerospace Standard | AIRCRAFT FIRE PROTECTION FOR RECIPROCATING AND GAS TURBINE ENGINE INSTALLATIONS |
Topic
Data Sets - Support Documents
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Issuing Committee
S-12 Powered Lift Propulsion Committee
Provides guidance and standardization for the better utilization of helicopter powerplants through studies of current practices in engine design, engine/airframe interface, and engine operation.
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| Number | Title |
|---|---|
| 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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