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MIL-STD-1290A, MILITARY STANDARD: LIGHT FIXED AND ROTARY WING AIRCRAFT CRASH RESISTANCE (26 SEPT 1988)

MIL-STD-1290A, MILITARY STANDARD: LIGHT FIXED AND ROTARY WING AIRCRAFT CRASH RESISTANCE (26 SEPT 1988)., This document establishes minimum crash resistance criteria for implementation in the initial stages of aircraft system design.

MIL-STD-1290 Rev. A

    

Version:
A01-200641.17 KB MIL-STD-1290A_NOTICE-2
A12-199517.97 KB MIL-STD-1290A_NOTICE-1
A09-19882.03 MB MIL-STD-1290A

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