MIL-A-008861A (NOTICE-1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (06-FEB-1986) [S/S BY MIL-A-87221]

MIL-A-008861A (NOTICE-1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (06-FEB-1986) [S/S BY MIL-A-87221]., Military specification MIL-A-008861A(USAF) dated 31 March 1971 is hereby canceled. For Air Force requirements, use MIL-A-87221 Aircraft Structures, General Specification For.