MIL-A-8866 › Historical Revision Information
Airplane Strength & Rigidity Reliability Requirements, Repeated Loads, Fatigue & Damag

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


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Document Number

MIL-A-8866

Revision Level

REVISION C

Status

Current

Publication Date

May 20, 1987

Page Count

15 pages