MIL-HDBK-1587 Base Document:1996
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
Available format(s)
PDF
Superseded date
06-21-2017
Superseded by
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.Establishes requirements for materials and processes used during design and production of aerospace weapon systems.
| Committee |
AREA MFFP
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| DevelopmentNote |
NOTICE 1 - Notice of Cancellation/Superseded by MIL STD 1587. (07/2017)
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| DocumentType |
Standard
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| Pages |
37
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy |
| 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) |
| 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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