MIL-A-002550C (AR), MILITARY SPECIFICATION, AMMUNITION, GENERAL SPECIFICATION FOR (17 NOV 1977)., This specification covers general requirements for all types of ammunition (non-nuclear and nuclear) and all components, propellants, explosives and other supplies used in or in support of ammunition.

MIL-A-101A (NOTICE 1), MILITARY SPECIFICATION, ADHESIVE, WATER-RESISTANT, FOR SEALING FIBERBOARD BOXES (11 OCT 1965) [S/S BY MMM-A-250C]., MIL-A–101A, dated 12 March 1952, is hereby canceled. Future procurement documents should cite Federal Specification MMM-A–250, Adhesive, Water-Resistant (For Sealing Fiberboard Boxes).

MIL-A-10450D, MILITARY SPECIFICATION, ANILINE, TECHNICAL (6 MAY 1983).,This specification covers one technical grade of aniline (C6H5NH2).

MIL-A-11356F, MILITARY SPECIFICATION, ARMOR, STEEL, CAST, HOMOGENEOUS, COMBAT-VEHICLE TYPE (1/4 TO 8 INCHES, INCLUSIVE) (22 MAY 1987)., This specification covers two classes of homogeneous cast steel armor, combat-vehicle type vehicles in thickness from 1/4 to 8 inches inclusive.

MIL-A-12560H (AMENDMENT 3), MILITARY SPECIFICATION, ARMOR PLATE , STEEL, WROUGHT, HOMOGENEOUS (FOR USE IN COMBAT-VEHICLES AND FOR AMMUNITION TESTING) (27 SEP 2000)., This amendment forms a part of MIL-A-12560H(MR), dated 28 November 1990, and is approved for use by the Army Research Laboratory, Department of the Army and is available for use by all Departments and Agencies of the Department of Defense.

MIL-A-12560H (w/INTERIM AMENDMENT 4), MILITARY SPECIFICATION, ARMOR PLATE , STEEL, WROUGHT, HOMOGENEOUS (FOR USE IN COMBAT-VEHICLES AND FOR AMMUNITION TESTING) (20 JUL 2007) [USED IN LIEU OF MIL-A-12560H (MR) w/AMENDMENT 3]., This specification is approved for use by all Departments and Agencies of the Department of Defense.

MIL-A-12560H, MILITARY SPECIFICATION, ARMOR PLATE , STEEL, WROUGHT, HOMOGENEOUS (FOR USE IN COMBAT-VEHICLES AND FOR AMMUNITION TESTING) (26 NOV 1990)., This specification covers wrought-steel homogeneous armor plate in thicknesses from 1/4 to 6 inches inclusive for use in combat-vehicles and 1/4 to 12 inches inclusive for use in proof and acceptance testing of armor defeating ammunition (see 6.1 and 6.4.3).

MIL-A-166C, MILITARY SPECIFICATION, AMMONIUM PICRATE (EXPLOSIVE D) (6 JAN 1975) [SUPERSEDING MIL-A-00166B (MU) & JAN-A-166A]., This specification covers one type of Ammonium Picrate (Explosive D) intended for use in ammunition.

MIL-A-17161D, MILITARY SPECIFICATION, ABSORBER, RADIO FREQUENCY RADIATION (MICROWAVE ABSORBING MATERIAL), GENERAL SPECIFICATION FOR (24 JUN 1985)., This specification covers the requirements for radio frequency (RF) radiation (microwave absorbing material (RAM) absorber, hereinafter referred to as RAM.

MIL-A-175C, MILITARY SPECIFICATION, AMMONIUM NITRATE, TECHNICAL (11 AUG 1983) [S/S by A-A-50460 and A-A-59476]., This specification covers two classes of technical grade ammonium nitrate.

MIL-A-18001K (w/ AMENDMENT 2), MILITARY SPECIFICATION, ANODES, SACRIFICIAL ZINC ALLOY (2 MAY 2005)., This specification covers the requirements for zinc anodes (galvanic protectors) in the form of plates, slabs, discs and rods for corrosion protection (cathodic protection) of metals and alloys. It also includes features of anode design and fabrication such as cast-in cores for mounting purposes. The material described by this specification contains elements for which the Occupational Safety and Health Administration (OSHA) has set standards for exposure limits. Handling, storage, and application of this material should be in accordance with the most recent Code of Federal Regulations Title 29, Part 1910 and 1915 and any other safety and health regulations (local or otherwise) which may apply.

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)., This specification covers three grades and seven classes of ammonium perchlorate.

MIL-A-19521B, MILITARY SPECIFICATION, ANODE RETAINING SUPPORT PLUGS AND ANODE SELECTION AND INSTALLATION DESIGN CRITERIA FOR SHIPBOARD CONDENSERS AND HEAT EXCHANGERS (4 MAY 1992)., This specification covers the threaded plugs used as support plugs for types ZRN and ZDM zinc anodes conforming to MIL-A-18001 and iron anodes. Appendix A of this specification establishes basic selection and installation criteria for the application of zinc (type ZEP, ZRN, and ZDM) and iron corrosion preventive anodes to copper, nickel, or iron alloy components of shipboard condensers and heat exchangers.

MIL-A-202C, MILITARY SPECIFICATION, ANTHRACENE, TECHNICAL (14 OCT 1981)., This specification covers two classes of technical grade anthracene (C14H10).

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, 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)., 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-22262B(SH) (AMENDMENT 2), MILITARY SPECIFICATION, ABRASIVE BLASTING MEDIA SHIP HULL BLAST CLEANING (21 MAR 1996)., This amendment forms a part of MIL-A-22262B(SH), dated 5 April 1993, and is approved for use by the Naval Sea Systems Command, Department of the Navy and is available for use by all Departments and Agencies of the Department of Defense.

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). 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-23121C (AS), MILITARY SPECIFICATION, AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM GENERAL SPECIFICATION FOR (23 JUN 1970)., This specification establishes the general requirements for the design, construction, installation, and performance of aircraft cockpit capsule aircrew environmental, escape and survival systems.

MIL-A-23442A (AMENDMENT 1), MILITARY SPECIFICATION, AMMONIUM PERCHLORATE (8 SEP 1966).

MIL-A-23442A, MILITARY SPECIFICATION, AMMONIUM PERCHLORATE (3 MAR 1965)., This specification covers the requirements for one grade of granular ammonium perchlorate.

MIL-A-23836, MILITARY SPECIFICATION, ANTENNA SYSTEMS, SUBMARINE, DESIGN, LOCATION, AND INSTALLATION, GENERAL SPECIFICATION (3 SEP 1963)., This specification covers the general mechanical and electrical requirements for design, and for location and installation on Submarines of antennas for electronic equipment, and is primarily for the use of antenna system manufacturers. Electronic equipment covered by this specification is primarily external to the pressure hull. In addition to the radiating elements (both active and passive), antenna systems within the scope of this specification consist of the radio-frequency transmission line from the connector at the inboard detecting or transmitting equipment to the outboard receiving or radiating element and all components which which serve to tune erect, protect or interconnect the antenna. The hydraulic system from the erecting mechanism back to the first distribution manifold is part of the system. Electrical control cables from the actuating equipment out to and including the outboard antenna components are part of the system. Functional parts of the submarine such as the snorkel tube and periscope which also serve as antenna masts shall conform to the requirements of their primary, purpose, suitably modified for subject multi-purpose use. The term system as employed within this specification refers to military operational function as a subsystem of a submarine rather than to electrical, electronic, mechanical and hydraulic equipment divisions. Antenna systems are essential for the safety and continued combat capability of the ship.

MIL-A-24319B (AMENDMENT 5), MILITARY SPECIFICATION, ANTENNA, WHIP, 10.67 METER (35 FEET), AS-2537 ( )/SR (24 JAN 1986).

MIL-A-24319B, MILITARY SPECIFICATION, ANTENNA, WHIP, 10.67 METER (35 FEET), AS-2537 ( )/SR (6 APR 1981)., This specification covers the design, performance of a two-piece 35 foot (ft) fiberglass reinforced plastic composite whip-type antenna ( hereinafter called the antenna) for use aboard surface ship and shore facilities for general communications purposes. This antenna is designed for transmit and receive operations over the 2,0000 through 29,9999 megahertz (MHz) frequency range and receive only operation over the 10-kilohertz (kHz) to 2,0000 MHz frequency range.

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-2550B (AMENDMENT 1), MILITARY SPECIFICATION, AMMUNITION, GENERAL SPECIFICATION FOR (24 APR 1973).

MIL-A-2550B, MILITARY SPECIFICATION, AMMUNITION, GENERAL SPECIFICATION FOR (8 FEB 1973)., This specification covers general requirements for all types of ammunition (non-nuclear and nuclear) and all components, propellants, explosives and other supplies used in ammunition.

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)., 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)., (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-46106B (AMENDMENT 3), MILITARY SPECIFICATION, ADHESIVE-SEALANTS, SILICONE, RTV, ONE-COMPONENT (26 JUN 1992)., This amendment forms a part of MIL-A-46106B, dated 11 December 1989, and is approved for use.

MIL-A-46106B, MILITARY SPECIFICATION, ADHESIVE-SEALANTS, SILICONE, RTV, ONE-COMPONENT (11 DEC 1989)., This specification covers three groups of one-part, room-temperature-vulcanizing (RTV), silicone adhesive-sealants which cure to durable, rubber adhesive-sealants upon reaction with moisture in the air. This specification also covers primers (see 6.1.3) for use with the silicone adhesive-sealants.

MIL-A-46146B (AMENDMENT 3), MILITARY SPECIFICATION, ADHESIVES-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) (28 OCT 1993)., This amendment forms a part of MIL-A-46146B, dated 21 November 1990 and is approved for use by all Departments and Agencies of the Department of Defense

MIL-A-46146B, MILITARY SPECIFICATION, ADHESIVES-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) (21 NOV 1990)., This specification covers three groups of one-part, room temperature-vulcanizing, non-fuel resistant, silicone compounds which cure to durable, rubber sealants and adhesives upon contact with moisture in the air. This specification also covers primers (see 6.1.3) for use with the silicone compounds.

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-46864B, MILITARY SPECIFICATION, ADHESIVE, EPOXY, MODIFIED, FLEXIBLE, TWO COMPONENT (28 MAR 1991) [S/S by A-A-56031]., This specification establishes the requirements for a two component modified epoxy adhesive system capable of curing at room temperature.

MIL-A-47040 (AMENDMENT 1), MILITARY SPECIFICATION, ADHESIVE-SEALANT, SILICONE, RTV, HIGH TEMPERATURE (4 OCT 1976) [S/S by MIL-A-46146].

MIL-A-47040 (NOTICE 1), MILITARY SPECIFICATION, ADHESIVE-SEALANT, SILICONE, RTV, HIGH TEMPERATURE (29 JUL 1991) [S/S by MIL-A-46146]., MIL-A-47040(MI), dated 26 April 1974, is hereby canceled. Future acquisition for this material should refer to MIL-A-46146, Adhesive-Sealants, Silicone, RTV, Noncorrosive (For Use With Sensitive Metals and Equipment).

MIL-A-47040, MILITARY SPECIFICATION, ADHESIVE-SEALANT, SILICONE, RTV, HIGH TEMPERATURE (26 APR 1974) [S/S by MIL-A-46146]., This specification covers one type of single package, high strength, thixotropic, vulcanizing silicone rubber for use in the -85 deg. F to +600 deg. F range.

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-6224E, MILITARY SPECIFICATION, ANTENNA SUBSYSTEM FOR UHF AIRBORNE COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR (7 JUN 1976)., This specification covers the general design, performance, and flight test requirements for an antenna subsystem used with UHF communication equipment in the frequency range of 22S to 400 MHz

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)., This specification covers the bonding of an aluminum plate to an aramid laminate pad to form a composite armor plate.

MIL-A-6271C, MILITARY SPECIFICATION, ANTENNA, VHF AIRBORNE COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN OF (7 JUN 1976)., This specification covers the general design, performance, and flight test requirements for an antenna subsystem used with VHF communication equipment in the frequency range of 118 to 156 MHz.

MIL-A-6300, MILITARY STANDARD, ANTENNA, OMNIDIRECTIONAL RECEIVING EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN OF (8 JAN 1951)., This specification covers the performance requirements for design of antennas for use with omni-directional range receiving equipment, including the furnishing of engineering reports.

MIL-A-6325, MILITARY SPECIFICATION, ANTENNAE, GLIDE PATH RADIO RECEIVING EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN OF (3 NOV 1950)., This specification covers the performance requirements for the design of antennae for use with glide path radio receiving equipment, including the furnishing of engineering reports.

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)., 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). 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-81573, MILITARY SPECIFICATION, MILITARY AIRCREW ESCAPE SYSTEM DATA PRESENTATIONS, SPECIFICATION DESCRIPTIVE AND PERFORMANCE REQUIREMENT AND FORMATS FOR; GENERAL SPECIFICATION FOR (1 APR 1968)., This specification defines escape systems and, in addition, establishes the data requirements for aircrew standard formats for (a) the presentation of data depicting aircrew escape system capabilities under varying conditions of speed, altitude, attitude, and sinkrate (b) system operation descriptions, and (c) system and ballistic component configuration. The formats established herein are compatible with the requirements for pilot’s handbooks and other publications, as herein specified.

MIL-A-81605D, MILITARY SPECIFICATION, ALTIMETER SET, ELECTRONIC AN/APN194(V) (5 DEC 1984)., This specification establishes the design performance and acceptance requirements for the AN/APN-194(v) Electronic Altimeter Set, herein referred to as the equipment. The equipment covered by this specification shall provide an accurate indication of absolute altitude of an aircraft at an altitude range of O to 5,000 feet over land and water. Altitude warnings are provided when the aircraft is at or below certain fixed or variable altitudes.

MIL-A-81815 (AS), MILITARY SPECIFICATION, AIRCREW AUTOMATED ESCAPE SYSTEMS, GENERAL SPECIFICATION FOR (31 MAY 1974)., This specification establishes (a) the general criteria to be used for selecting the type aircrew automated escape system for specific aircraft applications, (b) the general testing requirements for demonstrating escape system performance and conformance to specification requirements, and (c) the general escape system data requirements.

MIL-A-81973 (AS) (AMENDMENT 1), MILITARY SPECIFICATION, AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR (25 JUN 1974)., This amendment forms a part of Military Specification MIL-A-81973(AS) dated 31 MAY 1974, and has been approved by the Naval Air Systems Command, Department of the Navy.

MIL-A-81973 (AS), MILITARY SPECIFICATION, AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR (31 MAY 1974)., This specification establishes the requirements for the design, construction and instrumentation of track-type test vehicles used in performance/ service release testing, including underwater testing, of aircrew automated escape systems in accordance with the test requirements of MIL-E-9426.

MIL-A-83577B, ASSEMBLIES, MOVING, MECHANICAL FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR (1 FEB 1988)., 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-8421F (NOTICE 1), MILITARY SPECIFICATION, AIR TRANSPORTABILITY REQUIREMENTS, GENERAL SPECIFICATION FOR (28 MAY 1987) [S/S BY MIL-STD-1791]., MIL-A-8421F dated 25 October 1974 is hereby canceled. For future Air Force acquisition use development standard MIL-STD-1791 Designing for Internal Aerial Delivery in Fixed Wing Aircraft.

MIL-A-8576C, MILITARY SPECIFICATION, ADHESIVE, ACRYLIC BASE, FOR ACRYLIC PLASTIC (22 SEP 1984) [S/S by SAE-AMS-A-8576]., This specification covers acrylic-monomer base adhesives intended for use in bonding acrylic plastics.

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 (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. Future acquisition for these items should refer to MIL-STD-8591, “Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase).”

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 design criteria to which airborne stores, suspension equipment and their associated interfaces shall be designed. Provisions are included to promote cross-utilization and servicing capability among military aircraft of all services of the Department of Defense and various NATO country aircraft. Guidance is provided for design, analysis, test, and documentation of airborne stores, suspension equipment and the aircraft-store interface during captive operations. Acquisition of airborne stores and related suspension and release equipment shall be covered by a detail specification or drawing to be prepared by the contractor or acquiring activity.

MIL-A-8623A (NOTICE 1), MILITARY SPECIFICATION ADHESIVE, EPOXY RESIN, METAL TO METAL STRUCTURAL BONDING (7 JAN 1971) [S/S BY MMM-A-134].

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 (10 SEP 1993)., This specification covers the requirements for six types and two classes of electrolytically formed anodic coatings on aluminum and aluminum alloys for non-architectural applications (see 6.1).

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)., 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) [SUPERSEDES MIL-S-5700]., 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, 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 (6 may 1987)., 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 (19 JUL 1993)., 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-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. 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), 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, 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)., 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)., 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]., This specification covers the flight test requirements for the structural integrity flight and ground evaluation and demonstration of piloted airplanes.

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-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 airplanes.