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-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, 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, 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), 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), 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), MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (12 SEP 1967) [REFER TO MIL-STD-1789].
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), 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), 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), 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), 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, 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), 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, 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
MIL-A-8625D, MILITARY SPECIFICATION: ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS (30 JUN 1985)., This specification covers the requirements for six types andtwo classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for no
MIL-A-8591H (NOTICE 1), MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (12 DEC 2005) [S/S by MIL-STD-8591]., MIL-A-8591H(1), dated 30 June 1994, is hereby canceled.
MIL-A-8591H (AMENDMENT 1), MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (30 JUN 1994) [S/S by MIL-STD-8591].
MIL-A-8591H, MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (23 MAR 1990) [S/S by MIL-STD-8591]., This specification sets forth general structural and mechanical de
MIL-A-8591G (AMENDMENT 5), MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (14 AUG 1987) [S/S by MIL-STD-8591]., This amendment forms a part of Military Specificatio
MIL-A-8591G, MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (01 DEC 1983) [S/S by MIL-STD-8591]., This specification sets forth general structural and mechanical de
MIL-A-85802 (AS), MILITARY SPECIFICATION, ACTUATOR, ELECTROMECHANICAL, LINEAR (10 OCT 1986)., This specification establishes the requirements for themanufacture and inspection of one type of electromechanical linear actuator.The test limits in this specif
MIL-A-8576C, MILITARY SPECIFICATION: ADHESIVE, ACRYLIC BASE, FOR ACRYLIC PLASTIC (15 NOV 1997) [S/S by SAE-AMS-A-8576]., MIL-A-8576C, dated, is hereby canceled. Future acquisition for this sealing compound shouldrefer to Society Of Automotive Engineers (S
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
MIL-A-8625D
MIL-A-8625D, MILITARY SPECIFICATION: ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS (30 JUN 1985)., This specification covers the requirements for six types andtwo classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for no
MIL-A-8591H (NOTICE 1)
MIL-A-8591H (NOTICE 1), MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (12 DEC 2005) [S/S by MIL-STD-8591]., MIL-A-8591H(1), dated 30 June 1994, is hereby canceled.
MIL-A-8591H (AMENDMENT 1)
MIL-A-8591H (AMENDMENT 1), MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (30 JUN 1994) [S/S by MIL-STD-8591].
MIL-A-8591H
MIL-A-8591H, MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (23 MAR 1990) [S/S by MIL-STD-8591]., This specification sets forth general structural and mechanical de
MIL-A-8591G (AMENDMENT 5)
MIL-A-8591G (AMENDMENT 5), MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (14 AUG 1987) [S/S by MIL-STD-8591]., This amendment forms a part of Military Specificatio
MIL-A-8591G
MIL-A-8591G, MILITARY SPECIFICATION: AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE), GENERAL DESIGN CRITERIA FOR (01 DEC 1983) [S/S by MIL-STD-8591]., This specification sets forth general structural and mechanical de
MIL-A-85802 (AS)
MIL-A-85802 (AS), MILITARY SPECIFICATION, ACTUATOR, ELECTROMECHANICAL, LINEAR (10 OCT 1986)., This specification establishes the requirements for themanufacture and inspection of one type of electromechanical linear actuator.The test limits in this specif
MIL-A-8576C
MIL-A-8576C, MILITARY SPECIFICATION: ADHESIVE, ACRYLIC BASE, FOR ACRYLIC PLASTIC (15 NOV 1997) [S/S by SAE-AMS-A-8576]., MIL-A-8576C, dated, is hereby canceled. Future acquisition for this sealing compound shouldrefer to Society Of Automotive Engineers (S