MIL-A-9080

MIL-A-9080, MILITARY SPECIFICATION, ANTENNA, LIAISON COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN OF (2 FEB 1954)., This specification covers the performance requirements for the design of airborne antennas for use with liaison communication

MIL-A-907E (AMENDMENT 1)

MIL-A-907E (AMENDMENT 1), PERFORMANCE SPECIFICATION: ANTISEIZE THREAD COMPOUND, HIGH TEMPERATURE (13 JAN 1993) [S/S BY MIL-PRF-907F]., This amendment forms a part of MIL-A-907E, dated 18 June 1985, and is approved for use by the Naval Sea Systems Command,

MIL-A-907E (aka MIL-PRF-907E)

MIL-A-907E (aka MIL-PRF-907E), MILITARY SPECIFICATION: ANTISEIZE THREAD COMPOUND, HIGH TEMPERATURE (18 JUN 1985) [S/S BY MIL-PRF-907F]., This specification covers antiseize compound for use on threads of steel nuts, studs, bolts and other mating surfaces,

MIL-A-8892 (NOTICE 1)

MIL-A-8892 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY, VIBRATION (18 MAY 1987) [S/S BY MIL-A-87221]., MIL-A-8892(USAF) dated 31 March 1971 and amendment 1 dated 16 November 1971are hereby canceled. For future procurement, see MIL-

MIL-A-8882A (NOTICE 1)

MIL-A-8882A (NOTICE 1), MILITARY SPECIFICATION: ALUMINUM ALLOY PLATE AND SHEET, 2020 (06 DEC 1974) [NO S/S DOCUMENT]., Specification MIL-A-8882A (ASG), dated 29 March 1963, is hereby cancelled . The document is no longer required. There is nosuperseding d

MIL-A-8871A (NOTICE 1)

MIL-A-8871A (NOTICE 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (18 MAY 1987) [S/S BY MIL-A-87221]., MIL-A-8871A(USAF) dated 1 July 1971 is hereby canceled. For futureprocurements, see MIL-A-87221 Aircraft

MIL-A-8871A

MIL-A-8871A, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (01 JUL 1971) [S/S BY MIL-A-87221]., This specification covers the flight test requirements for the structural integrity flight and ground evaluation a

MIL-A-8870C

MIL-A-8870C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (25 MAR 1993)., This specification contains the general and detail designrequirements and criteria in the design and construction of airplanes to:a. Pre

MIL-A-8869B

MIL-A-8869B, MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS (20 MAY 1987)., This specification establishes the basic nuclear weapons effects requirements for airplanes which are Intended to deliver nuclear weapons or operate

MIL-A-8868B

MIL-A-8868B, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (20 MAY 1987)., This specification contains the requirements for data necessary to show compliance with the design and test requirements of MIL-A-8860 through MIL-A-8870

MIL-A-8868B (AMENDMENT 1)

MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24 MAY 1991).

MIL-A-8867C (AMENDMENT 1)

MIL-A-8867C (AMENDMENT 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993).

MIL-A-8867C

MIL-A-8867C, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (23 MAR 1987)., This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evalu

MIL-A-8866C (NOTICE 1)

MIL-A-8866C (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE (03 OCT 1994)., MIL-A-8866C(AS),dated 20 May 1987. has been reviewed and determined to bevalid for use i

MIL-A-8866C

MIL-A-8866C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE (20 MAY 1987)., This specification defines the strength and rigidity requirements for repeated loading condition ap

MIL-A-8865B

MIL-A-8865B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY, MISCELLANEOUS LOADS (20 MAY 1987) [SUPERSEDING MIL-S-5705]., This specification contains the strength and rigidity requirements for miscellaneous loads applicable to acquisition of airpl

MIL-A-8864 (NOTICE 1)

MIL-A-8864 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY WATER AND HANDLING LOADS FOR SEA PLANES (10 JUN 1982) [NO S/S DOCUMENT]., Specification MIL-A-8864 (ASG), dated 18 May 1960, is hereby canceled without replacement.

MIL-A-8863C

MIL-A-8863C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (19 JUL 1993)., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the follow

MIL-A-8863B

MIL-A-8863B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (06 MAY 1987)., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the follow

MIL-A-8861B (AMENDMENT 1)

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), dated7 February 1986, and is approved for use within the Naval Air SystemsCommand, Department of

MIL-A-8861B

MIL-A-8861B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (7 FEB 1986)., This specification covers the requirements for strength and rigidity for flight loading conditions applicable to airplanes.