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NPFC - MIL-STD-1290

LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE

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Organization: NPFC
Publication Date: 5 December 1995
Status: inactive
Page Count: 1

Document History

MIL-STD-1290
August 28, 2019
Light Fixed and Rotary-Wing Aircraft Crash Resistance
A description is not available for this item.
MIL-STD-1290
January 17, 2006
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
A description is not available for this item.
MIL-STD-1290
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...
MIL-STD-1290
July 21, 1977
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
A description is not available for this item.
MIL-STD-1290
January 25, 1974
LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
A description is not available for this item.
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References

This document is referenced by:
DEF STAN 00-970: PART 0 - Certification Specifications for Airworthiness Part 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Published by MODUK on March 14, 2021
Part 0 provides guidance and content information, together with definitions of terms used throughout this Standard.
This document is referenced by:
MIL-STD-3063 - ROTORCRAFT STRUCTURAL INTEGRITY PROGRAM (RSIP)
Published by NPFC on November 5, 2018
This standard practice describes the U.S. Army Rotorcraft Structural Integrity Program (RSIP), which defines the requirements necessary to substantiate and maintain structural integrity in U.S. Army...
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