MIL-A-8866 › Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance

MIL-A-8866 - REVISION C - CURRENT
Show Complete Document History

Included in this current edition are the following subparts:

 REVISION C - May 20, 1987
 REV C VALIDATION 1 - Oct. 3, 1994
 REV C VALIDATION 2 - July 9, 2019


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Document Number

MIL-A-8866

Revision Level

REVISION C

Status

Current

Publication Date

May 20, 1987

Page Count

15 pages