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MIL SPECS (MIL-A)
A-A-52313A, COMMERCIAL ITEM DESCRIPTION STEEL SHEETS, CORRUGATED: 2-1/2 INCH NOMINAL CORRUGATION,
A-A-52313A, COMMERCIAL ITEM DESCRIPTION STEEL SHEETS, CORRUGATED: 2-1/2 INCH NOMINAL CORRUGATION, PAINTED OR UNPAINTED (20 AUG 2006)., This commercial item description covers painted and unpainted corrugated steel sheets for roofing (type I) and siding (type II).
Ident. Num:
A-A-52313
Rev. Num:
A
A-A-52313A, COMMERCIAL ITEM DESCRIPTION STEEL SHEETS, CORRUGATED: 2-1/2 INCH NOMINAL CORRUGATION, PAINTED OR UNPAINTED (20 AUG 2006)., This commercial item description covers painted and unpainted corrugated steel sheets for roofing (type I) and siding (type II).
MIL-A-18455C (NOTICE 1), MILITARY SPECIFICATION ARGON, TECHNICAL (7 JUN 1991)
MIL-A-18455C (NOTICE 1), MILITARY SPECIFICATION ARGON, TECHNICAL (7 JUN 1991)., MIL-A-18455C, DATED 23 DECEMBER 1986, HAS BEEN REVIEWED AND DETERMINED TO BE VALID FOR ACQUISITION.
Ident. Num:
MIL-A-18455
Rev. Num:
C
MIL-A-18455C (NOTICE 1), MILITARY SPECIFICATION ARGON, TECHNICAL (7 JUN 1991)., MIL-A-18455C, DATED 23 DECEMBER 1986, HAS BEEN REVIEWED AND DETERMINED TO BE VALID FOR ACQUISITION.
MIL-A-192B, MILITARY SPECIFICATION AMMONIUM PERCHLORATE, TECHNICAL (2 SEP 1965)
MIL-A-192B, MILITARY SPECIFICATION AMMONIUM PERCHLORATE, TECHNICAL (2 SEP 1965)., This specification covers three grades and seven classes of ammonium perchlorate.
Ident. Num:
MIL-A-192
Rev. Num:
B
MIL-A-192B, MILITARY SPECIFICATION AMMONIUM PERCHLORATE, TECHNICAL (2 SEP 1965)., This specification covers three grades and seven classes of ammonium perchlorate.
MIL-A-21180D (AMENDMENT 1), MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (14 DEC 1991
MIL-A-21180D (AMENDMENT 1), MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (14 DEC 1991).
Ident. Num:
MIL-A-21180
Rev. Num:
D
MIL-A-21180D (AMENDMENT 1), MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (14 DEC 1991).
MIL-A-21180D (NOTICE 1), MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (10 SEP 1999)
MIL-A-21180D (NOTICE 1), MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (10 SEP 1999)., MIL-A-21180D, dated 5 November 1984, with Amendment 1, dated 14 December 1991, is hereby cancelled. Future acquisition for this item should refer to SAE-AMS-A-21180, "Aluminum-Alloy Castings, High Strength." (Application for copies of SAE Aerospace Material Specifications should be addressed to SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)
Ident. Num:
MIL-A-21180
Rev. Num:
D
MIL-A-21180D (NOTICE 1), MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (10 SEP 1999)., MIL-A-21180D, dated 5 November 1984, with Amendment 1, dated 14 December 1991, is hereby cancelled. Future acquisition for this item should refer to SAE-AMS-A-21180, "Aluminum-Alloy Castings, High Strength." (Application for copies of SAE Aerospace Material Specifications should be addressed to SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)
MIL-A-21180D, MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (5 NOV 1984)
MIL-A-21180D, MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (5 NOV 1984)., This specification covers the requirements for six alloy compositions, four inspection classes, four radiographic quality grades and six classes of mechanical properties of high strength aluminum-alloy castings.
Ident. Num:
MIL-A-21180
Rev. Num:
D
MIL-A-21180D, MILITARY SPECIFICATION ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH (5 NOV 1984)., This specification covers the requirements for six alloy compositions, four inspection classes, four radiographic quality grades and six classes of mechanical properties of high strength aluminum-alloy castings.
MIL-A-22771D (Notice 1), MILITARY SPECIFICATION, ALUMINUM ALLOY FORGINGS, HEAT TREATED (10 SEP 1999)
MIL-A-22771D (Notice 1), MILITARY SPECIFICATION, ALUMINUM ALLOY FORGINGS, HEAT TREATED (10 SEP 1999). MIL-A-22771D, dated 30 January 1984, is hereby cancelled. Future acquisition for this item should refer to SAE-AMS-A-22771, "Aluminum Alloy Forgings, Heat Treated." (Application for copies of SAE Aerospace Material Specifications should be addressed to SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)
Ident. Num:
MIL-A-22771
Rev. Num:
D
MIL-A-22771D (Notice 1), MILITARY SPECIFICATION, ALUMINUM ALLOY FORGINGS, HEAT TREATED (10 SEP 1999). MIL-A-22771D, dated 30 January 1984, is hereby cancelled. Future acquisition for this item should refer to SAE-AMS-A-22771, "Aluminum Alloy Forgings, Heat Treated." (Application for copies of SAE Aerospace Material Specifications should be addressed to SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)
MIL-A-22771D, MILITARY SPECIFICATION, ALUMINUM ALLOY FORGINGS, HEAT TREATED (30 JAN 1984)
MIL-A-22771D, MILITARY SPECIFICATION, ALUMINUM ALLOY FORGINGS, HEAT TREATED (30 JAN 1984). This specification covers the requirements for heat treated aluminum allow die forgings, hand forgings, and ring forgings, produced under additional mechanical property control to ensure known mechanical properteis for parts used in aerospace critical applications.
Ident. Num:
MIL-A-22771
Rev. Num:
D
MIL-A-22771D, MILITARY SPECIFICATION, ALUMINUM ALLOY FORGINGS, HEAT TREATED (30 JAN 1984). This specification covers the requirements for heat treated aluminum allow die forgings, hand forgings, and ring forgings, produced under additional mechanical property control to ensure known mechanical properteis for parts used in aerospace critical applications.
MIL-A-25487B, MILITARY SPECIFICATION ANTENNA AT-172()-ARN-14 (16 MAY 1987) (NO S/S DOCUMENT)
MIL-A-25487B, MILITARY SPECIFICATION ANTENNA AT-172()-ARN-14 (16 MAY 1987) (NO S/S DOCUMENT)., This specification covers the general mechanical and electrical requirements for design of an omnirange aircraft antenna for use in the frequency range of 108 to 122 MHz.
Ident. Num:
MIL-A-25487
Rev. Num:
B
MIL-A-25487B, MILITARY SPECIFICATION ANTENNA AT-172()-ARN-14 (16 MAY 1987) (NO S/S DOCUMENT)., This specification covers the general mechanical and electrical requirements for design of an omnirange aircraft antenna for use in the frequency range of 108 to 122 MHz.
MIL-A-28870A, MILITARY SPECIFICATION ASSEMBLIES, ELECTRICAL BACKPLANE, PRINTED-WIRING, GENERAL SPECIFICATION FOR (19 JAN 1990)
MIL-A-28870A, MILITARY SPECIFICATION ASSEMBLIES, ELECTRICAL BACKPLANE, PRINTED-WIRING, GENERAL SPECIFICATION FOR (19 JAN 1990)., This specification covers the general requirements for printed-wiring electrical backplane assemblies consisting of rigid printed-wiring boards on which separately manufactured compliant-component parts have been added.
Ident. Num:
MIL-A-28870
Rev. Num:
A
MIL-A-28870A, MILITARY SPECIFICATION ASSEMBLIES, ELECTRICAL BACKPLANE, PRINTED-WIRING, GENERAL SPECIFICATION FOR (19 JAN 1990)., This specification covers the general requirements for printed-wiring electrical backplane assemblies consisting of rigid printed-wiring boards on which separately manufactured compliant-component parts have been added.
MIL-A-3316C, MILITARY SPECIFICATION ADHESIVES, FIRE-RESISTANT, THERMAL INSULATION (20 OCT 1987)
MIL-A-3316C, MILITARY SPECIFICATION ADHESIVES, FIRE-RESISTANT, THERMAL INSULATION (20 OCT 1987)., This specification covers fire-resistant adhesives for securing cloth and tape to certain thermal insulations and for securing thermal insulations to metal surfaces.
Ident. Num:
MIL-A-3316
Rev. Num:
C
MIL-A-3316C, MILITARY SPECIFICATION ADHESIVES, FIRE-RESISTANT, THERMAL INSULATION (20 OCT 1987)., This specification covers fire-resistant adhesives for securing cloth and tape to certain thermal insulations and for securing thermal insulations to metal surfaces.
MIL-A-46100D (INTERIM AMENDMENT 2), MILITARY SPECIFICATION ARMOR PLATE, STEEL, WROUGHT, HIGH-HARNESS (13 JUL 2007)
MIL-A-46100D (INTERIM AMENDMENT 2), MILITARY SPECIFICATION ARMOR PLATE, STEEL, WROUGHT, HIGH-HARNESS (13 JUL 2007)., (All previous amendments incorporated)This specification covers quenched and tempered high-hardness wrought steel armor plate for lightweight armor applications for recommended thickness up to 2 inches inclusive (see 6.1 and 6.3).
Ident. Num:
MIL-A-46100
Rev. Num:
D
MIL-A-46100D (INTERIM AMENDMENT 2), MILITARY SPECIFICATION ARMOR PLATE, STEEL, WROUGHT, HIGH-HARNESS (13 JUL 2007)., (All previous amendments incorporated)This specification covers quenched and tempered high-hardness wrought steel armor plate for lightweight armor applications for recommended thickness up to 2 inches inclusive (see 6.1 and 6.3).
MIL-A-46153C, ANTIFREEZE, ETHYLENE GLYCOL, INHIBITED, HEAVY DUTY, SINGLE PACKAGE (31 JUL 1979) (S/S BY A-A-52624)
MIL-A-46153C, ANTIFREEZE, ETHYLENE GLYCOL, INHIBITED, HEAVY DUTY, SINGLE PACKAGE (31 JUL 1979) (S/S BY A-A-52624)., This specification covers one type of antifreeze compound for use in the cooling system of liquid-cooled internal combustion engines other than aircraft for protection against freezing in ambient temperatures as low as -51 deg. C.
Ident. Num:
MIL-A-46153
Rev. Num:
C
MIL-A-46153C, ANTIFREEZE, ETHYLENE GLYCOL, INHIBITED, HEAVY DUTY, SINGLE PACKAGE (31 JUL 1979) (S/S BY A-A-52624)., This specification covers one type of antifreeze compound for use in the cooling system of liquid-cooled internal combustion engines other than aircraft for protection against freezing in ambient temperatures as low as -51 deg. C.
MIL-A-50460A, AMMONIUM NITRATE, PRILLED (FOR USE IN AMMUNITION) (15 SEP 1973)
MIL-A-50460A, AMMONIUM NITRATE, PRILLED (FOR USE IN AMMUNITION) (15 SEP 1973)., This specification covers a high density phase-stabilized grade of prilled ammonium nitrate (NH 4 NO 3) for use in explosives.
Ident. Num:
MIL-A-50460
Rev. Num:
A
MIL-A-50460A, AMMONIUM NITRATE, PRILLED (FOR USE IN AMMUNITION) (15 SEP 1973)., This specification covers a high density phase-stabilized grade of prilled ammonium nitrate (NH 4 NO 3) for use in explosives.
MIL-A-62473A (AT), MILITARY SPECIFICATION ARMOR: ALUMINUM-ARAMID, LAMINATE-COMPOSITE (30 MAR 1954)
MIL-A-62473A (AT), MILITARY SPECIFICATION ARMOR: ALUMINUM-ARAMID, LAMINATE-COMPOSITE (30 MAR 1984)., This specification covers the bonding of an aluminum plate to an aramid laminate pad to form a composite armor plate.
Ident. Num:
MIL-A-62473
Rev. Num:
A
MIL-A-62473A (AT), MILITARY SPECIFICATION ARMOR: ALUMINUM-ARAMID, LAMINATE-COMPOSITE (30 MAR 1984)., This specification covers the bonding of an aluminum plate to an aramid laminate pad to form a composite armor plate.
MIL-A-62473B (AT), MILITARY SPECIFICATION ARMOR: ALUMINUM-ARAMID, LAMINATE-COMPOSITE (30 NOV 1992)
MIL-A-62473B (AT), MILITARY SPECIFICATION ARMOR: ALUMINUM-ARAMID, LAMINATE-COMPOSITE (30 NOV 1992)., This specification covers the bonding of an aluminum plate to an aramid laminate pad to form a composite armor plate.
Ident. Num:
MIL-A-62473
Rev. Num:
-
MIL-A-62473B (AT), MILITARY SPECIFICATION ARMOR: ALUMINUM-ARAMID, LAMINATE-COMPOSITE (30 NOV 1992)., This specification covers the bonding of an aluminum plate to an aramid laminate pad to form a composite armor plate.
MIL-A-63576A (AR) (NOTICE1), MILITARY SPECIFICATION ALUMINUM OXIDE COATING, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS (13 AUG 1998) (NO S/S DOCUME
MIL-A-63576A (AR)(NOTICE 1), MILITARY SPECIFICATION ALUMINUM OXIDE COATING, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS (13 AUG 1998) (NO S/S DOCUMENT)., MIL-A-63576A, dated 06 DECEMBER 1985, is hereby canceled without replacement.
Ident. Num:
MIL-A-63576
Rev. Num:
A
MIL-A-63576A (AR)(NOTICE 1), MILITARY SPECIFICATION ALUMINUM OXIDE COATING, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS (13 AUG 1998) (NO S/S DOCUMENT)., MIL-A-63576A, dated 06 DECEMBER 1985, is hereby canceled without replacement.
MIL-A-63576A (AR), MILITARY SPECIFICATION ALUMINUM OXIDE COATING, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS (6 DEC 1985)
MIL-A-63576A (AR), MILITARY SPECIFICATION ALUMINUM OXIDE COATING, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS (6 DEC 1985)., This specification covers the requirements for an electrochemical process for building a lubricative anodic coating on aluminum and aluminum alloys.
Ident. Num:
MIL-A-63576
Rev. Num:
A
MIL-A-63576A (AR), MILITARY SPECIFICATION ALUMINUM OXIDE COATING, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOYS (6 DEC 1985)., This specification covers the requirements for an electrochemical process for building a lubricative anodic coating on aluminum and aluminum alloys.
MIL-A-63576A (AR), MILITARY SPECIFICATION ALUMINUM OXIDE COATINGS, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOY (6 DEC 1985)
MIL-A-63576A (AR), MILITARY SPECIFICATION ALUMINUM OXIDE COATINGS, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOY (6 DEC 1985). This specification covers the requirements for an electrochemical process for building a lubricative anodic coating on aluminum and aluminum alloys. The unsealed anodic coating is impregnated with polytetrafluoroethylene (PTFE) or coated with a resin-bonded materials containing PTFE.
Ident. Num:
MIL-A-63576
Rev. Num:
A
MIL-A-63576A (AR), MILITARY SPECIFICATION ALUMINUM OXIDE COATINGS, LUBRICATIVE, FOR ALUMINUM AND ALUMINUM ALLOY (6 DEC 1985). This specification covers the requirements for an electrochemical process for building a lubricative anodic coating on aluminum and aluminum alloys. The unsealed anodic coating is impregnated with polytetrafluoroethylene (PTFE) or coated with a resin-bonded materials containing PTFE.
MIL-A-83577B, ASSEMBLIES, MOVING, MECHANICAL FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR
MIL-A-83577B, ASSEMBLIES, MOVING, MECHANICAL FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR. This specification sets forth the general e design, manufacture, quality control, and testing of moving mechanical assemblies to be used on space and launch vehicles.
Ident. Num:
MIL-A-83577
Rev. Num:
B
MIL-A-83577B, ASSEMBLIES, MOVING, MECHANICAL FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR. This specification sets forth the general e design, manufacture, quality control, and testing of moving mechanical assemblies to be used on space and launch vehicles.
MIL-A-8625F (AMENDMENT 1), MILITARY SPECIFICATION ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS (15 SEP 2003)
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 approved for use by all Departments and Agencies of the Department of Defense.
Ident. Num:
MIL-A-8625
Rev. Num:
F
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 approved for use by all Departments and Agencies of the Department of Defense.
MIL-A-8625F, MILITARY SPECIFICATION ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
MIL-A-8625F, MILITARY SPECIFICATION ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS.
Ident. Num:
MIL-A-8625
Rev. Num:
F
MIL-A-8625F, MILITARY SPECIFICATION ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS.
MIL-A-87135 (USAF), MILITARY SPECIFICATION, ADHESIVES, NON-CONDUCTIVE, FOR ELECTRONICS APPLICATIONS (16 FEB 1979)
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 to prevent vibration damage.
Ident. Num:
MIL-A-87135
Rev. Num:
-
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 to prevent vibration damage.
MIL-A-8806A, ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (11 JUL 1966)
MIL-A-8806A, ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (11 JUL 1966)., This specification covers the general requirements for the control of acoustical noise in occupied spaces of aircraft, including the acceptable noise levels and the testing requirements for determining conformance to these levels
Ident. Num:
MIL-A-8806
Rev. Num:
A
MIL-A-8806A, ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (11 JUL 1966)., This specification covers the general requirements for the control of acoustical noise in occupied spaces of aircraft, including the acceptable noise levels and the testing requirements for determining conformance to these levels
MIL-A-8860B, MILITARY SPECIFICATION AIRCRAFT STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR (20 MAY 1987)
MIL-A-8860B, MILITARY SPECIFICATION AIRCRAFT STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR (20 MAY 1987)., This specification contains general requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes.
Ident. Num:
MIL-A-8860
Rev. Num:
B
MIL-A-8860B, MILITARY SPECIFICATION AIRCRAFT STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR (20 MAY 1987)., This specification contains general requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes.
MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994)
MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994).
Ident. Num:
MIL-A-8861
Rev. Num:
B
MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994).
MIL-A-8861B, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (7 FEB 1986)
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.
Ident. Num:
MIL-A-8861
Rev. Num:
B
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-8863B (AS), AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
MIL-A-8863B (AS), AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the following ground loading conditions: a. Take-offs. b. Landings c. Ground maneuvering. d. Ground handling. e. Supplemental loads.
Ident. Num:
MIL-A-8863
Rev. Num:
B
MIL-A-8863B (AS), AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the following ground loading conditions: a. Take-offs. b. Landings c. Ground maneuvering. d. Ground handling. e. Supplemental loads.
MIL-A-8863C (AS), AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
MIL-A-8863C (AS), AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the following ground loading conditions: a. Take-offs. b. Landings c. Ground maneuvering. d. Ground handling. e. Supplemental loads.
Ident. Num:
MIL-A-8863
Rev. Num:
C
MIL-A-8863C (AS), AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the following ground loading conditions: a. Take-offs. b. Landings c. Ground maneuvering. d. Ground handling. e. Supplemental loads.
MIL-A-8865B, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY, MISCELLANEOUS LOADS (20 MAY 1987)
MIL-A-8865B, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY, MISCELLANEOUS LOADS (20 MAY 1987)., This specification contains the strength and rigidity requirements for miscellaneous loads applicable to acquisition of airplanes.
Ident. Num:
MIL-A-8865
Rev. Num:
-
MIL-A-8865B, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY, MISCELLANEOUS LOADS (20 MAY 1987)., This specification contains the strength and rigidity requirements for miscellaneous loads applicable to acquisition of airplanes.
MIL-A-8866C (AS) (NOTICE 1), MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLE
MIL-A-8866C (AS)(NOTICE 1), MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE. MIL-A-8866C(AS),dated 20 May 1987. has been reviewed and determined to be valid for use in acquisition
Ident. Num:
MIL-A-8866
Rev. Num:
C
MIL-A-8866C (AS)(NOTICE 1), MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE. MIL-A-8866C(AS),dated 20 May 1987. has been reviewed and determined to be valid for use in acquisition
MIL-A-8866C (AS), MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE
MIL-A-8866C (AS), MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE. This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes
Ident. Num:
MIL-A-8866
Rev. Num:
C
MIL-A-8866C (AS), MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE. This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes
MIL-A-8867C (AS) (AMENDMENT 1), MILITARY SPECIFICATION, AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993)
MIL-A-8867C (AS) (AMENDMENT 1), MILITARY SPECIFICATION, AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993).
Ident. Num:
MIL-A-8867
Rev. Num:
C
MIL-A-8867C (AS) (AMENDMENT 1), MILITARY SPECIFICATION, AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993).
MIL-A-8867C (AS), MILITARY SPECIFICATION, AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (23 MAR 1987)
MIL-A-8867C (AS), 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 evaluation of fixed wing piloted airplanes.
Ident. Num:
MIL-A-8867
Rev. Num:
C
MIL-A-8867C (AS), 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 evaluation of fixed wing piloted airplanes.
MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24 MAY 1991
MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24 MAY 1991).
Ident. Num:
MIL-A-8868
Rev. Num:
B
MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24 MAY 1991).
MIL-A-8868B, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (20 MAY 1987)
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 for the acquisition of naval airplanes, and to show the dependent relationship between the schedules for structural engineering analyses and testing and schedules for manufacturing.
Ident. Num:
MIL-A-8868
Rev. Num:
B
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 for the acquisition of naval airplanes, and to show the dependent relationship between the schedules for structural engineering analyses and testing and schedules for manufacturing.
MIL-A-8869B, MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS (20 MAY 1987)
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 in a nuclear conflict environment.
Ident. Num:
MIL-A-8869
Rev. Num:
B
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 in a nuclear conflict environment.
MIL-A-8870C, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (25 MAR 1993)
MIL-A-8870C, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (25 MAR 1993)., This specification contains the general and detail design requirements and criteria in the design and construction of airplanes to: a. Prevent flutter, divergence, and other dynamic and static aeroelastic instabilities. b. Control structural vibrations. c. Prevent fatigue failure of the airframe structure or structural components induced by vibrations, aeroacoustic and other oscillatory loads for the service life of the airplane. d. Prescribe structural dynamic analyses, laboratory and ground tests, and structural dynamic flight tests required to demonstrate compliance with design requirements. e. Apply to airplanes acquired by the Navy for all conditions of flight and surface operations for which the airplanes are required to operate.
Ident. Num:
MIL-A-8870
Rev. Num:
C
MIL-A-8870C, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (25 MAR 1993)., This specification contains the general and detail design requirements and criteria in the design and construction of airplanes to: a. Prevent flutter, divergence, and other dynamic and static aeroelastic instabilities. b. Control structural vibrations. c. Prevent fatigue failure of the airframe structure or structural components induced by vibrations, aeroacoustic and other oscillatory loads for the service life of the airplane. d. Prescribe structural dynamic analyses, laboratory and ground tests, and structural dynamic flight tests required to demonstrate compliance with design requirements. e. Apply to airplanes acquired by the Navy for all conditions of flight and surface operations for which the airplanes are required to operate.
MIL-A-8871A, MILITARY SPECIFICATION, AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (1 JUL 1971) [S/S BY MIL-A-87221]
MIL-A-8871A, MILITARY SPECIFICATION, AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (1 JUL 1971) [S/S BY MIL-A-87221]., This specification covers the flight test requirements for the structural integrity flight and ground evaluation and demonstration of piloted airplanes.
Ident. Num:
MIL-A-8871
Rev. Num:
A
MIL-A-8871A, MILITARY SPECIFICATION, AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (1 JUL 1971) [S/S BY MIL-A-87221]., This specification covers the flight test requirements for the structural integrity flight and ground evaluation and demonstration of piloted airplanes.
