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

MIL-A-8861 - BASE - SUPERSEDED
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Airplane Strength and Rigidity Flight Loads


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FSC 1510 (Aircraft, Fixed Wing)

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Document Number

MIL-A-8861

Revision Level

BASE

Status

Superseded

Publication Date

May 18, 1960

Page Count

19 pages