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

MIL-A-8861 - REV B AMENDMENT 1 - CURRENT
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Airplane Strength and Rigidity Flight Loads


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Document Number

MIL-A-8861

Revision Level

REV B AMENDMENT 1

Status

Current

Publication Date

Dec. 5, 1994

Page Count

1 page