MIL-A-8861 Historical Revision Information
Airplane Strength and Rigidity Flight Loads

MIL-A-8861 - REVISION B - CURRENT
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Airplane Strength and Rigidity Flight Loads


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Document Number

MIL-A-8861

Revision Level

REVISION B

Status

Current

Publication Date

Feb. 7, 1986

Page Count

33 pages