MIL-A-8866C
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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 applicable to Navy procured airplanes
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 applicable to Navy procured airplanes
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 in acquisition
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 evaluation of fixed wing piloted airplanes.
MIL-A-8867C (AMENDMENT 1)
MIL-A-8867C (AMENDMENT 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993).
MIL-A-8868B (AMENDMENT 1)
MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24 MAY 1991).
MIL-A-8868B
MIL-A-8868B, MILITAR! Y SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPOR! TS (20 M AY 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
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
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. Prevent flutter, divergence, and other dynamic and staticaeroelastic instabilities.b. Control structural vibrations.c. Prevent fatigue failure of the airframe structure or structuralcomponents 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
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 gro! und evaluation and demonstration of piloted airplanes.
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 Structures, General Specification For.
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 document.
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 am! endment 1 dated 16 November 1971are hereby canceled. For future procurement, see MIL-A-87221 AircraftStructures, General Specification For.
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, including those of superheated steam installations, at temperatures up to 1050 degrees Fahrenheit (degrees F) (566 degrees Celsius (degrees C)).
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! , Department of the Navy, and is available for use by all Depa! rtments and Agencies of the Department
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 equipment, including the furnishing of engineering reports
MIL-A-9117D
MIL-A-9117D, MILITARY SPECIFICATION: ADHESIVE; SEALING, FOR AROMATIC FUEL CELLS AND GENERAL REPAIR (19 APR 1971) [S/S BY MIL-PRF-9117E]., This specification covers a one-part sealing adhesive for fuel cell repair workand for other general repairs where resistance to aromatic fuel is required.
MIL-A-9962A
MIL-A-9962A, MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (01 DEC 1966) [S/S BY S/S by A-! A-58054]., This specification covers non-woven, non-metallic mats made of nylon fiber which are bonded together with waterproof adhesives containing abrasives.
MIL-A-9962A (AMENDMENT 4)
MIL-A-9962A (AMENDMENT 4), MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (05 APR 1977) [S/S by A-A-58054]., This amendment forms a of Military Specification MIL-A-9962A, dated 1 December 1966, and is approved for use by all Departments and Agencies of the Department of Defe.rise
MIL-A-9962A (NOTICE 1)
MIL-A-9962A (NOTICE 1), MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (05 APR 1996) [S/S by A-A-58054]., MIL-A-9962A (4), dated 5 APRIL 1977, is hereby canceled. Future acquisitions should be made using the current revision of A-A-58054.
MIL-A-8806B
MIL-A-8! 806B, MILITARY SPECIFICATION: SOUND PRESSURE LEVELS IN AIRCRAF! T, GENER AL SPECIFICATION FOR (21 SEP 1970) [MIL-S-008806B USED IN LIEU OF MIL-A-8806A] [S/S BY MIL-STD-1789]., This specification covers the general requirements for maximum allowable sound pressure levels in aircraft crew and passenger compartments and the testing requirements for determining conformance to these levels.
http://www.infoeach.com/item-1643.html
恭颂商祺 万事如意
---------------------------------------------------------------------
世界资料网提供各种行业资料， 国军标、 美军标、 美国汽车工程师协会 SAE、 美国材料测试协会 ASTM、 情报专利 期刊 、 会议论文、 统计数据、 海关资料数据 年鉴、 行业数据、 协会数据、 政府报告、 商务部报告等。
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Email: ke...@infoeach.com
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 applicable to Navy procured airplanes
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 applicable to Navy procured airplanes
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 in acquisition
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 evaluation of fixed wing piloted airplanes.
MIL-A-8867C (AMENDMENT 1)
MIL-A-8867C (AMENDMENT 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993).
MIL-A-8868B (AMENDMENT 1)
MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24 MAY 1991).
MIL-A-8868B
MIL-A-8868B, MILITAR! Y SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPOR! TS (20 M AY 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
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
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. Prevent flutter, divergence, and other dynamic and staticaeroelastic instabilities.b. Control structural vibrations.c. Prevent fatigue failure of the airframe structure or structuralcomponents 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
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 gro! und evaluation and demonstration of piloted airplanes.
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 Structures, General Specification For.
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 document.
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 am! endment 1 dated 16 November 1971are hereby canceled. For future procurement, see MIL-A-87221 AircraftStructures, General Specification For.
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, including those of superheated steam installations, at temperatures up to 1050 degrees Fahrenheit (degrees F) (566 degrees Celsius (degrees C)).
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! , Department of the Navy, and is available for use by all Depa! rtments and Agencies of the Department
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 equipment, including the furnishing of engineering reports
MIL-A-9117D
MIL-A-9117D, MILITARY SPECIFICATION: ADHESIVE; SEALING, FOR AROMATIC FUEL CELLS AND GENERAL REPAIR (19 APR 1971) [S/S BY MIL-PRF-9117E]., This specification covers a one-part sealing adhesive for fuel cell repair workand for other general repairs where resistance to aromatic fuel is required.
MIL-A-9962A
MIL-A-9962A, MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (01 DEC 1966) [S/S BY S/S by A-! A-58054]., This specification covers non-woven, non-metallic mats made of nylon fiber which are bonded together with waterproof adhesives containing abrasives.
MIL-A-9962A (AMENDMENT 4)
MIL-A-9962A (AMENDMENT 4), MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (05 APR 1977) [S/S by A-A-58054]., This amendment forms a of Military Specification MIL-A-9962A, dated 1 December 1966, and is approved for use by all Departments and Agencies of the Department of Defe.rise
MIL-A-9962A (NOTICE 1)
MIL-A-9962A (NOTICE 1), MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (05 APR 1996) [S/S by A-A-58054]., MIL-A-9962A (4), dated 5 APRIL 1977, is hereby canceled. Future acquisitions should be made using the current revision of A-A-58054.
MIL-A-8806B
MIL-A-8! 806B, MILITARY SPECIFICATION: SOUND PRESSURE LEVELS IN AIRCRAF! T, GENER AL SPECIFICATION FOR (21 SEP 1970) [MIL-S-008806B USED IN LIEU OF MIL-A-8806A] [S/S BY MIL-STD-1789]., This specification covers the general requirements for maximum allowable sound pressure levels in aircraft crew and passenger compartments and the testing requirements for determining conformance to these levels.
http://www.infoeach.com/item-1643.html
恭颂商祺 万事如意
---------------------------------------------------------------------
世界资料网提供各种行业资料， 国军标、 美军标、 美国汽车工程师协会 SAE、 美国材料测试协会 ASTM、 情报专利 期刊 、 会议论文、 统计数据、 海关资料数据 年鉴、 行业数据、 协会数据、 政府报告、 商务部报告等。
网址:http://www.infoeach.com
Email: ke...@infoeach.com
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