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.

MIL-A-8860B

MIL-A-8860B, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR (20 MAY 1987) [SUPERSEDES MIL-S-5700]., This specification contains general requirements, which, in combination with other applicable specifications, define the

MIL-A-8836B (NOTICE 1)

MIL-A-8836B (NOTICE 1), MILITARY SPECIFICATION: ABBREVIATED SUMMARY BILL OF MATERIALS FOR ITEMS IN DEPARTMENTS OF THE ARMY, NAVY, AND AIR FORCE CONTRACTS (18 MAY 1987) [S/S BY MIL-STD-295]., MIL-A-8836 dated 30 April 1971 and amendment 2 dated 22 January

MIL-A-8806A (NOTICE 1)

MIL-A-8806A (NOTICE 1), MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (10 SEP 1997) [REFER TO MIL-STD-1789]., This notice should be filed in front of MIL-A-8806A, dated 11 July 1966, and Amendment-1, dated 12 Septem

MIL-A-8806A (AMENDMENT 1)

MIL-A-8806A (AMENDMENT 1), MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (12 SEP 1967) [REFER TO MIL-STD-1789].

MIL-A-8806A

MIL-A-8806A, MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (11 JUL 1966) [REFER TO MIL-STD-1789]., This specification covers the general requirements for the control of acoustical noise in occupied spaces of aircraf

MIL-A-87244A (NOTICE 1)

MIL-A-87244A (NOTICE 1), AVIONICS/ELECTRONICS INTEGRITY PROGRAM REQUIREMENTS (AVIP) (30 JAN 1995) [S/S BY MIL-HDBK-87244]., MIL-A-87244a (USAF) is hereby cancelled. Future program should use MIL-HDBK-87244 (USAF), Avionics/Electronics Integrity.

MIL-A-87221 (NOTICE 1)

MIL-A-87221 (NOTICE 1), MILITARY SPECIFICATION: AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR (8 JUN 1990) [S/S by AFGS-87221]. ML-A-87221, dated 28 February 1985, is hereby canceled. Future acquisitions should refer to AFGS-87221A.

MIL-A-87135 (USAF)

MIL-A-87135 (USAF), MILITARY SPECIFICATION, ADHESIVES, NON-CONDUCTIVE, FOR ELECTRONICS APPLICATIONS (16 FEB 1979)., This specification establishes requirements for a moderately fast curing adhesive used for bonding components to printed-wiring assemblies

MIL-A-8625F (AMENDMENT 1)

MIL-A-8625F (AMENDMENT 1), MILITARY SPECIFICATION: ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS (15 SEP 2003)., This amendment forms a part of MIL-A-8625F, dated 10 September 1993, and is approvedfor use by all Departments and Agencies of the Departme

MIL-A-8625F

MIL-A-8625F, MILITARY SPECIFICATION: ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS (10 SEP 1993)., This specification covers the requirements for six types andtwo classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for no

MIL-A-8625E (AMENDMENT 1)

MIL-A-8625E (AMENDMENT 1), MILITARY SPECIFICATION: ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS (13 NOV 1989).,This amendment forms a Dart of military specification MIL-A-8625E.dated 25 April 1988, and is approved far use by all Departments and Agenci

MIL-A-8625E

MIL-A-8625E, MILITARY SPECIFICATION: ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS (25 APR 1988)., This specification covers the requirements for six types andtwo classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for no