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MIL SPECS (MIL-H)


Ident. Num:
MIL-H-15021 
  Rev. Num:

MIL-H-15021A (AMENDMENT 2), MILITARY SPECIFICATION, HOOKS, SNAP BOLT, SWIVEL-EYE, AND RINGS (4 NOV 1959)., This amendment forms a part of Military Specification MIL-H-15021A, 28 November 1950 has been approved by the Department of Defense, and is mandatory for use by the Departments of the Army, the Navy and the Air Force.
Ident. Num:
MIL-H-15317 
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MIL-H-15317C, MILITARY SPECIFICATION, HOISTS, CHAIN OR WIRE ROPE, ELECTRIC POWER OPERATED, LUG, HOOK, OR TROLLEY SUSPENSION AND BASE MOUNTED (16 FEB 1982)., This specification covers electrical power-driven hoists and trolleys.
Ident. Num:
MIL-H-17660D 
  Rev. Num:

MIL-H-17660D (NOTICE 1), MILITARY SPECIFICATION, HEATERS, FLUID DEAERATING (FOR WATER ONLY) 1,000 TO 1,600,000 POUNDS PER HOUR CAPACITY (2 JUNE 1997)., Military Specification MIL-H-17660D, dated 18 June 1993, is hereby canceled. Future acquisition of this material should refer to Federal Specification W-H-2904.
Ident. Num:
MIL-H-18911 
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MIL-H-18911A, MILITARY SPECIFICATION, HEADS AND MOTORS, ROCKET, INERT PARTS, PAINTING AND MARKING (27 FEB 1974)., This specification covers the painting and marking of all types of rocket heads and motors by the manufacturer of inert parts.
Ident. Num:
MIL-H-21040 
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MIL-H-21040C, MILITARY SPECIFICATION, HONEYCOMB MATERIALS, WATER MIGRATION RESISTANT TYPE, STRUCTURAL, PAPER BASE (16 JUL 1974)., This specification covers fully cured, resin-treated, kraft paper, water migration resistant type honeycomb materials for structural applications
Ident. Num:
MIL-H-22868 

MIL-H-22868 (WEP), MILITARY SPECIFICATION HYDROGEN PEROXIDE, E-STABILIZED, 70% AND 90% (FOR TORPEDO USE). This specification covers aqueous solutions of hydrogen peroxide in which additives have been dissolved to impart a low decomposition rate, to repress the effects of an accidental catalytic contamination, and to prevent corrosion of aluminum containers. Such hydrogen peroxide solutions are designated as "E" stabilized.
Ident. Num:
MIL-H-25475 
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MIL-H-25475B, MILITARY SPECIFICATION, HYDRAULIC SYSTEMS, MISSILE DESIGN, INSTALLATION AND TESTS, GENERAL REQUIREMENTS FOR (29 APR 1971)., This specification covers the design, installation, and testing of missile hydraulic systems.
Ident. Num:
MIL-H-25579 
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MIL-H-25579E, MILITARY SPECIFICATION HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, HIGH TEMPERATURE, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR (24 JAN 1985)., This specification contains the requirements for medium pressure, high temperature, polytetrafluoroethylene (PTFE) hose assemblies, reinforced with a corrosion-resistant steel (CRES) wire braid for use in fuel, lubricating oil, water-alcohol, hydraulics and pneumatic systems within the limits specified herein.
Ident. Num:
MIL-H-26626 
  Rev. Num:

MIL-H-26626D, MILITARY SPECIFICATION HOSE ASSEMBLY, REINFORCED, CRYOGENIC, OXYGEN (1 NOV 1991)., This specification covers reinforced cryogenic oxygen hose assemblies with flared tube style fittings.
Ident. Num:
MIL-H-27856 
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MIL-H-27856D, MILITARY SPECIFICATION, HELMET, FLYING HGU-7/P (8 MAY 1981)., This specification covers one type of flyer's helmet with a removable sunshade and headset-microphone H-256/AIC. The helmet is designated HGU-7/P and is furnished in small, medium, and large sizes as specified (see 6.2).
Ident. Num:
MIL-H-2813 
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MIL-H-2813B, HOISTS, CHAIN AND WIRE ROPE, PNEUMATIC (17 aug 1974)., This specification covers pneumatic powered chain and wire rope hoists
Ident. Num:
MIL-H-28693 

MIL-H-28693(YD), MILITARY SPECIFICATION, HOSE, RUBBER, OIL AND GASOLINE DISCHARGE, SMOOTH BORE, LIGHTWEIGHT BUOYANT TYPE, LONGITUDINALLY REINFORCED, 6 INCH (29 MAR 1993)., This specification covers a 6-inch, lightweight, smooth bore, longitudinally reinforced oil and gasoline discharge rubber hose, furnished with couplings and a hose support ring. The system is intended for use as part of a buoyant fueling system. The maximum working pressure of this hose is 150 pound-force per square inch (psi).
Ident. Num:
MIL-H-3780C 
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MIL-H-3780, MILITARY SPECIFICATION, HANGER & TRACK SETS, HORIZONTAL SLIDING DOOR-(5 MAR 1976) [S/S BY BHMA A156.14]., This specification covers steel tracks, hangers, brackets, and hardware for horizontal sliding doors.
Ident. Num:
MIL-H-3982 
  Rev. Num:

MIL-H-3982C, MILITARY SPECIFICATION, HARDWARE (FASTENERS AND RELATED ITEMS), PACKAGING AND PACKING FOR SHIPMENT AND STORAGE OF (6 MAY 1969) [S/S BY PPP-H-1581].
Ident. Num:
MIL-H-43895 
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MIL-H-43895B (NOTICE 1), MILITARY SPECIFICATION, HEATERS, HOT WATER BOOSTER, ELECTRIC; SINK, SANITIZING (18 DEC 1992)., MIL-H-43895B, dated 24 June, 1986, has been reviewed and determined to be valid for use in acquisition.
Ident. Num:
MIL-H-43964 
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MIL-H-43964, MILITARY SPECIFICATION, HONEYCOMB CORE, NON-METALLIC, SHELTER PANELS (31 MAR 1977)., This specification covers the requirements for non-metallic honeycomb core for shelter panel applications
Ident. Num:
MIL-H-46855 
  Rev. Num:

MIL-H-46855B (AMENDMENT 1), MILITARY SPECIFICATION, HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT AND FACILITIES (5 APR 1984) [S/S BY MIL-STD-46855].
Ident. Num:
MIL-H-46855 
  Rev. Num:

MIL-H-46855B, MILITARY SPECIFICATION, HUMAN ENGINEERING REQUIREMENTS FOR MILITARY SYSTEMS, EQUIPMENT AND FACILITIES (31 JAN 1979) [S/S BY MIL-STD-46855]., This specification establishes and defines the requirements for applying human engineering to the development and acquisition of military systems, equipment and facilities. These requirements include the work to be accomplished by the contractor or subcontractor in conducting a human engineering effort integrated with the total system engineering and development effort. These requirements are the basis for including human engineering during proposal preparation, system analysis, task analysis, system design (including computer software design), equipment and facilities design, testing, and documentation and reporting.
Ident. Num:
MIL-H-5440 
  Rev. Num:

MIL-H-5440H (SUPPLEMENT 1), MILITARY SPECIFICATION, HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION, REQUIREMENTS FOR (25 MAY 1993) [S/S BY SAE-AS5440]., This supplement forms a part of MIL-H-5440H dated 25 May 1993.
Ident. Num:
MIL-H-5440 
  Rev. Num:

MIL-H-5440H, MILITARY SPECIFICATION HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR (25 MAY 1993)., This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems.
Ident. Num:
MIL-H-5440 
  Rev. Num:

MIL-H-5440H, MILITARY SPECIFICATION, HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION, REQUIREMENTS FOR (25 MAY 1993) [S/S BY SAE-AS5440]., This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems.
Ident. Num:
MIL-H-55053 
  Rev. Num:

MIL-H-55053B, MILITARY SPECIFICATION, HARDWARE, POLE LINE (27 MAR 1962) [SUPERSEDING MIL-H-19320]., This specification covers hardware as used in the construction of pole lines, towers, etc.
Ident. Num:
MIL-H-5606 
  Rev. Num:

MIL-H-5606G, PERFORMANCE SPECIFICATION HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE (9 SEP 1994)., This specification describes the characteristics and provides the requirements for a petroleum base hydraulic fluid for use in the -54°C to +135°C temperature range (see 6.1). This fluid is identified by military symbol OHA and NATO Code No. H-515 (see 6.5).
Ident. Num:
MIL-H-6000 
  Rev. Num:

MIL-H-6000B, DETAIL SPECIFICATION HOSE, RUBBER, AIRCRAFT, FUEL, OIL, COOLANT, WATER, AND ALCOHOL (22 MAR 1982)., This specification covers one type of hose for use in fuel, oil, coolant, water, and for alcohol lines in engine installations.
Ident. Num:
MIL-H-6088 
  Rev. Num:

MIL-H-6088G (AMENDMENT 1), MILITARY SPECIFICATION HEAT TREATMENT OF ALUMINUM ALLOYS (15 SEP 1992) (S/S BY SAE-AMS-H-6088).
Ident. Num:
MIL-H-6088 
  Rev. Num:

MIL-H-6088G, MILITARY SPECIFICATION HEAT TREATMENT OF ALUMINUM ALLOYS (1 APR 1991) (S/S BY SAE-AMS-H-6088)., This specification covers the requirements and recommendations for the heat treatment of aluminum alloy rolled, extruded, forged, drawn, and cast product (see 6.1 and 6.5.1). It does not cover the requirements for the heat treatment of aluminum alloy parts (see 3.4).
Ident. Num:
MIL-H-6875 
  Rev. Num:

MIL-H-6875H (AMENDMENT 1), MILITARY SPECIFICATION HEAT TREATMENT OF STEEL, PROCESS FOR (16 JULY 1993)., This amendment forms a part of MIL-H-6875H, dated 1 March 1989, and is approved for use by all Departments and Agencies of the Department of Defense.
Ident. Num:
MIL-H-6875 
  Rev. Num:

MIL-H-6875H (AMENDMENT 2), MILITARY SPECIFICATION HEAT TREATMENT OF STEEL, PROCESS FOR (27 OCT 1998)., This amendment forms a part of MIL-H-6875H, dated 1 March 1989, and is approved for use by all Departments and Agencies of the Department of Defense.
Ident. Num:
MIL-H-6875 
  Rev. Num:

MIL-H-6875H (NOTICE 1), MILITARY SPECIFICATION HEAT TREATMENT OF STEEL RAW MATERIALS (2 FEB 1999) (S/S BY SAE-AMS-H-6875)., Mil-H-6875H, dated 1 March 198 9, along with amendment 2 dated 27 October 1998, is hereby cancelled. Future acquisitions should refer to SAE-AMS-H-6875, “Heat Treatment of Steel raw materials.” (Applications for copies of SAE publications should be addressed to the Society of Automotive Engineers, 400 Commonwealth Drive, Warrendale, PA 15096-0001).
Ident. Num:
MIL-H-6875 
  Rev. Num:

MIL-H-6875H, MILITARY SPECIFICATION HEAT TREATMENT OF STEEL, PROCESS FOR (1 MAR 1989)., This specification covers the requirements for heat-treatment of four classes of steel (see 1.2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (see 6.11) test procedures.
Ident. Num:
MIL-H-7195 
  Rev. Num:

MIL-H-7195G (NOTICE 1), MILITARY STANDARD, HARDWARE, PARACHUTE, GENERAL SPECIFICATION FOR (8 AUG 1998) [S/S BY PIA-H-7195]., MIL-H-7195G, dated 07 October 1991, is hereby canceled without replacement.
Ident. Num:
MIL-H-7195 
  Rev. Num:

MIL-H-7195G (NOTICE 2), MILITARY STANDARD, HARDWARE, PARACHUTE, GENERAL SPECIFICATION FOR (31 MAY 2005) [S/S BY PIA-H-7195]., MIL-H-7195G, dated 7 October 1991, is hereby canceled. Future acquisition for this material should refer to PIA-H-7195, "HARDWARE, PARACHUTE, GENERAL SPECIFICATION FOR". Users are cautioned to evaluate the replacement for their particular application. (Copies of these documents are available online at http://www.pia.com/ or from the Parachute Industry Association, 3833 West Oakton Street, Skokie, IL 60076.)
Ident. Num:
MIL-H-7195 
  Rev. Num:

MIL-H-7195G, MILITARY SPECIFICATION, HARDWARE, PARACHUTE, GENERAL SPECIFICATION FOR (7 OCT 1991) [S/S BY PIA-H-7195]., This specification covers the general requirements for all types of parachute hardware (see 6.4.1).
Ident. Num:
MIL-H-81200 
  Rev. Num:

MIL-H-81200B, MILITARY SPECIFICATION HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS (13 JAN 1991) (S/S BY SAE-AMS-H-81200B)., This specification covers the heat treatment of titanium and titanium alloy products, including wrought and cast products, by material producers. This specification also covers furnace equipment requirements, test procedures, and general information for heat treating procedures, heat treating temperatures, and material test procedures for the heat treatment of titanium and titanium alloys.
Ident. Num:
MIL-H-83282 
  Rev. Num:

MIL-H-83282C, PERFORMANCE SPECIFICATION HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 (25 MAR 1986) (S/S BY MIL-PRF-83282D)., This specification covers the requirements for a synthetic hydrocarbon-base hydraulic fluid for use in the temperature range of -40° to +205°C. This hydraulic fluid is identified by NATO Code Number H-537 (see 6.6).
Ident. Num:
MIL-H-8501 
  Rev. Num:

MIL-H-8501A (AMENDMENT 1), MILITARY SPECIFICATION, HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (3 APR 1962)., This amendment forms a part of Military Specification MIL-H-8601A, 7 September 1961, and has been approved by the Department of Defense and is mandatory for use by the Departments of the Army, the Navy, and the Air Force.
Ident. Num:
MIL-H-8501 
  Rev. Num:

MIL-H-8501A (NOTICE 1), MILITARY SPECIFICATION, HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (20 JUN 1972).
Ident. Num:
MIL-H-8501 
  Rev. Num:

MIL-H-8501A (NOTICE 2), MILITARY SPECIFICATION, HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (16 AUG 1995).
Ident. Num:
MIL-H-8501 
  Rev. Num:

MIL-H-8501A, MILITARY SPECIFICATION, HELICOPTER FLYING AND GROUND HANDLING QUALITIES, GENERAL REQUIREMENTS FOR (7 SEP 1961)., This specification covers the design requirements for flying and ground handling qualities of U.S. military helicopters.
Ident. Num:
MIL-H-87990 
  Rev. Num:

MIL-H-87990 (AMENDMENT 1), ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES, MANUFACTURE OF (15 FEB 1992).
Ident. Num:
MIL-H-87990 
  Rev. Num:

MIL-H-87990, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES, MANUFACTURE OF (18 DEC 1989)., This specification covers the requirements for fabrication and acceptance of adhesive bonded, aluminum faced, non-perforated aluminum honeycomb core, sandwich assemblies intended for use as aircraft spare parts.
Ident. Num:
MIL-H-8891 
  Rev. Num:

MIL-H-8891A, HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES, TYPE III DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR (23 JAN 1978)., This specification covers the design and installation requirements for Type III manned flight vehicle hydraulic systems.
Ident. Num:
MIL-H-904 
  Rev. Num:

MIL-H-904J (NOTICE 1), MILITARY SPECIFICATION, HOISTS, CHAIN, HAND-OPERATED, HOOK AND TROLLEY SUSPENSION (18 FEB 2003)., MIL-H-904J is inactive for new design and is no longer used, except for replacement purposes. Future acquisitions for new design of MIL-H-904J should be made under ASME HST-3, "Performance Standard for Manually Lever Operated Chain Hoists".
Ident. Num:
MIL-J-24445 
  Rev. Num:

MIL-J-24445A, MILITARY SPECIFICATION, JOINT, BIMETALLIC BONDED, ALUMINUM TO STEEL (25 JUL 1977)., This specification covers aluminum to steel transition joints made by the roll bonding and explosion processes. The joints are obtained from aluminum to steel bonded plate, and may be supplied in various geometries such as bars, discs, rings, or rectangles. This specification does not cover joints made by welding or brazing.
Ident. Num:
MIL-J-43923 
  Rev. Num:

MIL-J-43923C, MILITARY SPECIFICATION, JACKET, FLYER'S, LIGHTWEIGHT, (EXPANDABLE WRISTS AND WAIST) (13 APR 1990)., This specification covers a self-lined jacket made of a high temperature resistant aramid oxford cloth.
Ident. Num:
MIL-J-83382 
  Rev. Num:

MIL-J-83382C (AMENDMENT 1), MILITARY SPECIFICATION, JACKET, FLYER'S, MEN'S, (1 NOV 1985).
Ident. Num:
MIL-J-83382 
  Rev. Num:

MIL-J-83382C, MILITARY SPECIFICATION, JACKET, FLYER'S, MEN'S, (30 OCT 1981)., This specification covers one type of flight jacket. The jacket is designated CWU-36/P.
Ident. Num:
MIL-J-83388 
  Rev. Num:

MIL-J-83388E, MILITARY SPECIFICATION, JACKET, FLYER'S, COLD WEATHER (18 JUN 1992)., This specification contains the requirements for the CWU-45/P cold weather flyer's jacket and hood, detachable.



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