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MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994)

MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994)., This amendment forms a part of MIL-A-886lB(AS), dated 7 February 1986, and is approved for use within the Naval Air Systems Command, Department of the Navy, and is available for use by all Departments and Agencies of the Department of Defense.

MIL-A-8861 Rev. B

    
 Status:
Active

 FSC Code:
 1510 - Aircraft, Fixed Wing

Version:
B07-20192.02 KB MIL-A-8861B_NOTICE-1
B12-199434.21 KB MIL-A-8861B_AMENDMENT-1
B02-19861.63 MB MIL-A-8861B

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