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  • MIL-HDBK-1587 Base Document:1996

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM

    Available format(s):  PDF

    Superseded date:  21-06-2017

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    Establishes requirements for materials and processes used during design and production of aerospace weapon systems.

    General Product Information - (Show below) - (Hide below)

    Committee AREA MFFP
    Development Note NOTICE 1 - Notice of Cancellation/Superseded by MIL STD 1587. (07/2017)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    MIL-STD-186 Revision F:2002 PROTECTIVE FINISHING SYSTEMS FOR ROCKETS, GUIDED MISSILES, SUPPORT EQUIPMENT AND RELATED MATERIALS
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    JSSG-2009 Revision A:2013 Air Vehicle Subsystems
    SAE AS 4073 : 2013(R2018) AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES
    MIL-STD-1530 Revision D:2016 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP)

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-I-81550 Revision C:1983 INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE
    MIL-R-83248 Revision C:1994 RUBBER, FLUOROCARBON ELASTOMER, HIGH TEMPERATURE, FLUID, AND COMPRESSION SET RESISTANT
    MIL HDBK 5 : G_VOL2 METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
    MIL-M-24041 Revision C:1981 MOLDING AND POTTING COMPOUND
    MIL-S-9041 Revision B:1975 SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND HONEYCOMB CORE FOR AIRCRAFT STRUCTURAL APPLICATIONS
    ASTM E 1 : 2014 : REDLINE Standard Specification for ASTM Liquid-in-Glass Thermometers
    AWS D1.2 : 1997 STRUCTURAL WELDING CODE - ALUMINUM
    NAS1514:2011 RADIOGRAPHIC STANDARD FOR CLASSIFICATION OF FUSION WELD DISCONTINUITIES
    MIL-STD-129 Revision R:2014 Military Marking for Shipment and Storage
    MIL-A-46146 Revision B:1990 ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT)
    MIL R 25988/4 : 0 RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 80
    MIL-P-5315 Revision B:1964 PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT
    MIL-STD-970 Base Document:1987 STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF
    MIL-A-83377 Revision B:1978 ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR
    MIL C 8073 : D CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED CLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS
    MIL-R-83485 Base Document:1976 RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    SAE AMS 2770 : 2015 HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS
    MIL-T-81556 Revision A:1983 TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY
    MIL-A-22771 Revision D:1984 ALUMINUM ALLOY FORGINGS, HEAT TREATED
    MIL R 6855 : E RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES
    MIL-STD-1783 Base Document:1984 ENGINE STRUCTURAL INTEGRITY PROGRAM (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503)
    MIL R 25988/1 : A RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 70
    MIL-C-27725 Revision B:1969 COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS
    MIL-S-8802 Revision F:1990 SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION
    QQ-A-367 Revision H:1973 ALUMINUM ALLOY FORGINGS
    SAE AMS 2759 : 2014 HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS
    SAE AMS 2301 : 2015 STEEL CLEANLINESS, AIRCRAFT QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE
    SAE AS 568 : 2014 AEROSPACE SIZE STANDARD FOR O-RINGS
    MIL-T-9046 Revision J:1983 TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE
    MIL-STD-2175 Revision A:1993 CASTING, CLASSIFICATION AND INSPECTION OF
    MS29513 Revision C:1966 PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, O RING
    MIL-E-47231 Base Document:1974 ELECTRICAL COMPONENTS, POTTING OF
    MIL-HDBK-275 Revision A:1976 GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS
    MIL R 83248/1 : A RUBBER, FLUOROCARBON ELASTOMER, HIGH TEMPERATURE, FLUID AND COMPRESSION SET RESISTANT (O-RINGS, CLASS 1, 75 HARDNESS)
    MIL-STD-889 Revision C:2016 DISSIMILAR METALS
    MIL R 25988/2 : 0 RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 3
    MIL-C-7438 Revision G:1985 CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION
    MIL-STD-866 Revision C:2007 Grinding of Chrome Plated Steel and Steel Parts Heat Treated to 180,000 PSI or Over
    MS28778 Revision C:1984 PACKING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS
    MS28775 Revision E:1984 PACKING, PREFORMED, HYDRAULIC, PLUS 275 DEG. F. (O RING)
    SAE AMS 2750 : 2012 PYROMETRY
    MIL R 25988/3 : 0 RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 60
    MIL S 13165 : C SHOT PEENING OF METAL PARTS
    MS29512 Revision C:1965 PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT TUBE FITTING 0 RING
    MIL-F-7190 Revision B:1985 FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS
    MIL-STD-838 Revision C:1983 LUBRICATION OF MILITARY EQUIPMENT
    MIL-STD-1595 Revision A:1982 QUALIFICATION OF AIRCRAFT, MISSILE AND AEROSPACE FUSION WELDERS
    SAE AMS 3100 : 2013 ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS
    MIL I 6870 : E INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
    MIL-A-46106 Revision B:1989 ADHESIVE-SEALANTS, SILICONE, RTV, ONE-COMPONENT
    MIL S 8516 : F SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED
    MIL-STD-2219 Revision A:2005 FUSION WELDING FOR AEROSPACE APPLICATIONS
    MIL R 25988 : B RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES
    MIL-STD-1568 Revision D:2015 Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems
    MIL-STD-2000 Revision A:1991 STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES
    SAE AMS 2303 : 2016 STEEL CLEANLINESS, AIRCRAFT QUALITY, MARTENSITIC CORROSION-RESISTANT STEELS, MAGNETIC PARTICLE INSPECTION PROCEDURE
    MIL A 87244 : A NOTICE 1 AVIONICS ELECTRONICS INTEGRITY PROGRAM REQUIREMENTS
    MIL R 83397 : A RUBBER, POLYURETHANE, CASTABLE, HUMIDITY RESISTANT
    FED-STD-191 Revision A:1978 TEXTILE TEST METHODS
    MIL-B-7883 Revision B:1968 BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS
    MIL-STD-1523 Revision A:1984 AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL
    MIL S 23586 : E SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED
    MIL STD 1807 : NOTICE 1 CRASH SURVIVABILITY OF AIRCRAFT PERSONNEL
    MIL-A-21180 Revision D:1984 ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
    MIL T 83483 : B THREAD COMPOUND, ANTISEIZE, MOLYBDENUM DISULFIDE-PETROLATUM
    MIL C 8087 : C CORE MATERIAL, FOAMED IN PLACE, URETHANE TYPE
    MIL-S-81732 Base Document:1969 SEALING COMPOUND, ELECTRICAL, HIGH STRENGTH, ACCELERATOR REQUIRED
    SAE AMS 5343 : 2014 STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB (NB) - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H1000), 150 KSI (1034 MPA) TENSILE STRENGTH (17-4)
    MIL-H-6088 Revision G:1991 HEAT TREATMENT OF ALUMINIUM ALLOYS
    MS29561 Revision A:1966 PACKING, PREFORMED, O RING, SYNTHETIC LUBRICANT RESISTANT
    MIL-W-6858 Revision D:1978 WELDING RESISTANCE, SPOT AND SEAM
    SAE AMS 2300 L : 2015 STEEL CLEANLINESS, PREMIUM AIRCRAFT-QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE
    SAE AMS 3856 : 2016 CLOTH, UPHOLSTERY, FLAME RESISTANT
    AWS D1.1 : 2000 STRUCTURAL WELDING CODE - STEEL
    MIL-P-83461 Revision B:1980 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C)
    MIL-I-16923 Revision H:1991 INSULATING COMPOUND, ELECTRICAL, EMBEDDING, EPOXY
    ZZ-R-765 Revision E:1991 RUBBER, SILICONE; RUBBER SHEET SOLID
    MIL-STD-1798 Revision C:2013 MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    MIL-W-6873 Revision C:1991 WELDING FLASH CARBON AND ALLOY STEEL
    MIL-F-83142 Revision A:1969 FORGING, TITANIUM ALLOYS, PREMIUM QUALITY
    MIL-S-25392 Revision B:1968 SANDWICH CONSTRUCTION, PLASTIC RESIN, GLASS FABRIC BASE, LAMINATED FACINGS AND POLYURETHANE FOAMED-IN-PLACE CORE, FOR AIRCRAFT STRUCTURAL APPLICATIONS
    MIL-P-83461-1 Revision B:1989 PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT IMPROVED PERFORMANCE OF 275 DEG. F (135 DEG. C) SIZES AND TOLERANCES
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