NPFC - MIL-STD-1290
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
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| Organization: | NPFC |
| Publication Date: | 26 September 1988 |
| Status: | active |
| Page Count: | 46 |
scope:
Purpose. This document establishes minimum crash resistance criteria for implementation in the initial stages of aircraft system design.
Classification. The requirements of this specification pertain to the following aircraft types:
Type I - Light Fixed-Wing
Type II - Rotary-wing, including Tilt Prop/Rotor Aircraft
Document History
August 28, 2019
Light Fixed and Rotary-Wing Aircraft Crash Resistance
A description is not available for this item.
January 17, 2006
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
A description is not available for this item.
December 5, 1995
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
A description is not available for this item.
MIL-STD-1290
September 26, 1988
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
Purpose. This document establishes minimum crash resistance criteria for implementation in the initial stages of aircraft system design.
Classification. The requirements of this specification...
July 21, 1977
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
A description is not available for this item.
January 25, 1974
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
A description is not available for this item.
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