NAVY MIL-A-8861 B (1)-1994
AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS [Use In Lieu Of: NAVY MIL-A-008861 A CANC NOTICE]

Standard No.

NAVY MIL-A-8861 B (1)-1994

Release Date

1994

Published By

United States Navy

Scope

This amendment forms a part of MIL-A-8861B(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.