MIL-A-8861 › Airplane Strength and Rigidity Flight Loads

MIL-A-8861 - REVISION B - CURRENT
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Included in this current edition are the following subparts:

 REVISION B - Feb. 7, 1986
 REV B AMENDMENT 1 - Dec. 5, 1994
 REV B VALIDATION 1 - July 9, 2019


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Document Number

MIL-A-8861

Revision Level

REVISION B

Status

Current

Publication Date

Feb. 7, 1986

Page Count

33 pages