MIL-STD-1587 Revision D:2017
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
Available format(s)
PDF
Superseded date
14-05-2021
Superseded by
Language(s)
English
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
Sets up the requirements for materials and processes used during design and production of aerospace weapons systems.
| Committee |
AREA MFFP
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| DevelopmentNote |
Supersedes MIL HDBK 1587. (07/2017)
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| DocumentType |
Standard
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| Pages |
34
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| MIL-M-8856 Revision B:1990 | MISSILE, GUIDED, STRUCTURAL INTEGRITY, GENERAL SPECIFICATION FOR |
| MIL-F-87154 Base Document:1980 | FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
| MIL-T-83823 Base Document:1991 | TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
| MIL-T-83965 Revision B:1990 | TRUCK, FIRE FIGHTING, A/S32P-10, FORCIBLE ENTRY |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| AFGS-87154 Revision A:1992 | FUEL SYSTEMS, GENERAL DESIGN SPECIFICATION FOR |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-P-87210 Base Document:1984 | PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
| MIL-E-87236 Base Document:1985 | |
| MIL-I-87216 Base Document:1984 | INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
| MIL-C-83821 Base Document:1990 | CRANE, WHEEL MOUNTED, CRASH, ROUGH TERRAIN, HYDRAULIC FULL REVOLVING, 4X4, DED, FIGHTER TYPE AIRCRAFT |
| MIL A 87221 : 0 | AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| AFGS 87145 : A NOTICE 1 | ENVIRONMENTAL CONTROL, AIRBORNE |
| MIL-C-5584 Revision D:1988 | CONTAINER, SHIPPING AND STORAGE, METAL REUSABLE |
| MIL-O-87226 Base Document:1985 | OXYGEN SYSTEMS, AIRCRAFT |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL-M-38795 Revision B:1982 | MANUAL, TECHNICAL, SYSTEM PECULIAR CORROSION CONTROL PREPARATION OF. |
| MIL-L-87139 Base Document:1979 | LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-S-87238 Base Document:1985 | SURVIVAL AND FLOTATION SYSTEM, AIRBORNE |
| MIL-HDBK-1568 Base Document:1996 | MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
| JSSG-2010-10 Base Document:1998 | Crew Systems Oxygen Systems Handbook |
| MIL-STD-1944 Base Document:1985 | POLYMER MATRIX COMPOSITES |
| 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 |
| SAE AMS6910B | Titanium Alloy Bars, Forgings and Forging Stock 8Al - 1Mo - 1V Duplex Annealed |
| SAE AMSA21180B | Aluminum-Alloy Castings, High Strength |
| SAE AMSS8802D | Sealing Compound, Fuel Resistant, Integral Fuel Tanks and Fuel Cell Cavities |
| SAE AMS6925B | Titanium Alloy Bars, Forgings and Forging Stock 13V - 11Cr - 3Al Solution Heat Treated |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| SAE AMSC27725D | Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C) |
| 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 |
| SAE AS 29512 : 2016 | HYDROCARBON FUEL RESISTANT, TUBE FITTING, O-RING MOLDED FROM AMS-P-5315 RUBBER |
| SAE AMS6900B | Titanium Alloy Bars, Forgings and Forging Stock 5Al - 2.5Sn Annealed |
| ISO 15614-13:2012 | Specification and qualification of welding procedures for metallic materials Welding procedure test Part 13: Upset (resistance butt) and flash welding |
| SAE AMS4940B | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 25.0 ksi (172 MPa) Yield Strength |
| SAE AMS4915L | Titanium Alloy Sheet, Strip, and Plate 8Al - 1V - 1Mo Single Annealed |
| SAE AMS6932B | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al – 4.0V Extra Low Interstitial Annealed |
| SAE AMS4911N | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
| SAE AS81550A | Insulating Compound, Electrical, Embedding, Reversion Resistant Silicone |
| ASTM B 265 : 2015 : REDLINE | Standard Specification for Titanium and Titanium Alloy Strip, Sheet, and Plate |
| SAE AMSP5510A | O-Ring, Preformed, Straight Thread Tube Fitting Boss, Type I Hydraulic (-65 to 160 °F) |
| SAE AMS4989C | Titanium Alloy Sheet, Strip, and Plate 3Al - 2.5V Annealed |
| SAE AMS 2175 : 2010 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| MIL-DTL-83397 Revision B:2009 | RUBBER, POLYURETHANE, CASTABLE, HUMIDITY RESISTANT |
| SAE AMSR83285A | Rubber, Ethylene-Propylene, General Purpose |
| MIL-PRF-23586 Revision F:1996 | Sealing Compound (With Accelerator), Silicone Rubber, Electrical |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AMS2770M | Heat Treatment of Wrought Aluminum Alloy Parts |
| SAE AS28775A | PACKING, PREFORMED - MS28775 O-RING |
| MIL-T-81556 Revision A:1983 | TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
| AWS C3.7M/C3.7 : 2011 | SPECIFICATION FOR ALUMINUM BRAZING |
| SAE AMS C 8073 : 2013 | CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED GLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS |
| SAE AS3581 | PACKING, PREFORMED – O-RING SEAL AMS7259 |
| SAE AMS4918N | Titanium Alloy, Sheet, Strip, and Plate 6Al - 6V - 2Sn Annealed |
| SAE AMS6921B | Titanium Alloy Bars, Forgings and Forging Stock 3Al - 8V - 6Cr - 4Mo - 4Zr Solution Heat Treated and Aged |
| SAE AMS7276H | Rubber: Fluorocarbon (FKM) High-Temperature-Fluid Resistant Low Compression Set For Seals In Fuel Systems and Specific Engine Oil Systems |
| SAE AS3208 | PACKING, PREFORMED - AMS 7276 - SEAL |
| AWS C3.6M/C3.6 : 2016 | SPECIFICATION FOR FURNACE BRAZING |
| SAE AMS4990C | Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated and Aged |
| SAE AMS4919H | Titanium Alloy Sheet, Strip, and Plate 6Al - 2Sn - 4Zr - 2Mo - 0.08Si Duplex Annealed |
| SAE AMS6905B | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo Duplex Annealed |
| SAE AMS3216G | Fluorocarbon (FKM) Rubber High-Temperature - Fluid Resistant Low Compression Set 70 to 80 |
| AWS D1.2/D1.2M : 2014 | STRUCTURAL WELDING CODE - ALUMINUM |
| MIL R 25988/1 : A | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 70 |
| SAE AMS4902K | Titanium Sheet, Strip, and Plate Commercially-Pure Annealed 40.0 ksi (276 MPa) Yield Strength |
| SAE AMS3384 | Rubber, Fluorocarbon Elastomer (FKM) 70 to 80 Hardness, Low Temperature Sealing Tg -22 °F (-30 °C) For Elastomeric Shapes or Parts in Gas Turbine Engine Oil, Fuel and Hydraulic Systems |
| SAE AMS6940A | Titanium Alloy Bars, Forgings and Forging Stock 3.0Al - 2.5V Annealed |
| SAE AMSA22771C | Aluminum Alloy Forgings, Heat Treated |
| JSSG-2010 Base Document:1998 | Crew Systems |
| SAE AMS2759E | Heat Treatment of Steel Parts General Requirements |
| AWS C3.5M/C3.5 : 2016 | SPECIFICATION FOR INDUCTION BRAZING |
| SAE AMS2301K | Steel Cleanliness, Aircraft Quality Magnetic Particle Inspection Procedure |
| SAE AMSP83461 | Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C) |
| SAE AS568D | Aerospace Size Standard for O-rings |
| MIL-HDBK-275 Revision A:1976 | Guide for Selection of Lubricants, Fluids, and Compounds for Use in Flight Vehicles and Components |
| SAE AMS2430T | Shot Peening, Automatic |
| SAE AMS6907B | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo Duplex Annealed |
| SAE AMS6915B | Titanium Alloy Bars, Forgings and Forging Stock 7.0Al - 4.0Mo Annealed |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| AWS D17.2/D17.2M : 2013 | SPECIFICATION FOR RESISTANCE WELDING FOR AEROSPACE APPLICATIONS |
| MIL R 25988/2 : 0 | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 3 |
| SAE AMS4917H | Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated |
| SAE AMS6931C | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Annealed |
| AWS C3.4M/C3.4 : 2016 | SPECIFICATION FOR TORCH BRAZING |
| A-A-59588 Revision B:2012 | Rubber, Silicone |
| MIL-STD-866 Revision C:2007 | Grinding of Chrome Plated Steel and Steel Parts Heat Treated to 180,000 PSI or Over |
| SAE AS1933A | Age Controls for Hose Containing Age-Sensitive Elastomeric Material |
| SAE AMSQQA367D | Aluminum Alloy Forgings |
| SAE AMS2750E | Pyrometry |
| MIL R 25988/3 : 0 | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 60 |
| SAE AMS6926B | Titanium Alloy Bars, Forgings and Forging Stock 13V - 11Cr - 3Al Solution Heat Treated and Aged |
| SAE AMS7287 | Fluorocarbon Elastomer (FKM) High Temperature / HTS Oil Resistant / Fuel Resistant Low Compression Set / 70 to 80 Hardness, Low Temperature Tg -22 °F (-30 °C) For Seals in Oil / Fuel / Specific Hydraulic Systems |
| SAE AS83461/2B | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
| SAE AMS6920C | Titanium Alloy Bars, Forgings and Forging Stock 3Al - 8V - 6Cr - 4Mo - 4Zr Solution Heat Treated |
| SAE AMS3100D | Adhesion Promoter For Polysulfide Sealing Compounds |
| SAE AMSR7362A | Nitrile Rubber, Synthetic, Solid, Sheet, Strip and Fabricated Parts, Synthetic Oil Resistant |
| SAE ARP5316D | Storage of Elastomer Seals and Seal Assemblies Which Include an Elastomer Element Prior to Hardware Assembly |
| SAE AMS7259E | Rubber: Fluorocarbon (FKM) High Temperature/Fluid Resistant Low Compression Set/85 to 95 Hardness For Seals In Fuel Systems and Specific Engine Oil Systems |
| MIL-A-46106 Revision B:1989 | ADHESIVE-SEALANTS, SILICONE, RTV, ONE-COMPONENT |
| SAE AMS4910R | Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed |
| MIL-HDBK-83377 Base Document:1997 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for |
| SAE AMS4907K | Titanium Alloy, Sheet, Strip, and Plate 6.0Al - 4.0V, Extra Low Interstitial Annealed |
| SAE AMS2772G | Heat Treatment of Aluminum Alloy Raw Materials |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE AMS2303F | Steel Cleanliness, Aircraft Quality Martensitic Corrosion-Resistant Steels Magnetic Particle Inspection Procedure |
| MIL-PRF-83483 Revision E:2014 | ANTISEIZE THREAD COMPOUND, MOLYBDENUM DISULFIDE-PETROLATUM |
| SAE AMS4921N | Titanium Bars, Wire, Forgings, and Rings Commercially Pure 70 ksi (483 MPa) Yield Strength |
| SAE AMS4988C | Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated |
| FED-STD-191 Revision A:1978 | TEXTILE TEST METHODS |
| SAE AMSH81200D | Heat Treatment of Titanium and Titanium Alloys |
| SAE AMS3218C | Fluorocarbon (FKM) Rubber High-Temperature-Fluid Resistant Low Compression Set 85 to 95 |
| SAE AS83461/1B | M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
| SAE AS29561B | O-RING, SYNTHETIC LUBRICANT RESISTANT MOLDED FROM AMS-R-7362 RUBBER |
| SAE AS28778B | O-RING, STRAIGHT THREAD TUBE FITTING BOSS MOLDED FROM AMS-P-5510 RUBBER |
| SAE AMS4904C | Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated and Aged |
| SAE AMS4909K | Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn, Extra Low Interstitial Annealed |
| SAE AMS6906B | Titanium Alloy Bars, Forgings, and Forging Stock 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo Solution Heat Treated and Aged |
| SAE AS50881F | Wiring Aerospace Vehicle |
| SAE AMS5343E | 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) |
| SAE AMSF7190B | Forging, Steel, For Aircraft/Aerospace Equipment and Special Ordnance Applications |
| MIL-HDBK-838 Base Document:1997 | LUBRICATION OF MILITARY EQUIPMENT |
| A-A-59877 Base Document:2010 | Insulating Compound, Electrical, Embedding |
| MIL-PRF-8516 Revision G:1997 | SEALING COMPOUND, SYNTHETIC RUBBER, ELECTRIC CONNECTORS AND ELECTRIC SYSTEMS, CHEMICALLY CURED |
| SAE AMS4903C | Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated |
| SAE AMS2300L | Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure |
| SAE AMS3856B | Cloth, Upholstery, Flame Resistant |
| SAE AMS6930E | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Solution Heat Treated and Aged |
| SAE AMS4916K | Titanium Alloy Sheet, Strip, and Plate 8Al - 1Mo - 1V Duplex Annealed |
| SAE AS3209 | PACKING, PREFORMED - AMS 7276, \'O\' RING |
| SAE AMSP5315B | Acrylonitrile-butadiene (NBR) Rubber For Fuel-Resistant Seals 60 to 70 |
| AWS D1.1/D1.1M : 2015 | STRUCTURAL WELDING CODE-STEEL |
| MIL-PRF-6855 Revision F:2009 | RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES, GENERAL SPECIFICATION FOR |
| MIL-HDBK-6870 Revision B:2012 | NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| MIL-DTL-25988 Revision C:2006 | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES |
| SAE AMS6936B | Titanium Alloy Bars, Forgings and Forging Stock 6Al - 6V - 2Sn Annealed |
| SAE AMS6935B | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al – 6.0V – 2.0Sn Solution Heat Treated and Aged |
| MIL-STD-1798 Revision C:2013 | MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| ASTM E 162 : 2016 : REDLINE | Standard Test Method for Surface Flammability of Materials Using a Radiant Heat Energy Source |
| SAE AMS C 7438 : 2014 | CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
| AWS D17.1/D17.1M : 2012 | SPECIFICATION FOR FUSION WELDING FOR AEROSPACE APPLICATIONS |
| SAE AMS6901B | Titanium Alloy Bars, Forgings, and Forging Stock 5Al - 2.5Sn, Extra Low Interstitial Annealed |
| SAE AS 29513 : 2016 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, 'O' RING |
| SAE AMS4901T | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| 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 |
| SAE AMS4900P | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 55 ksi (379 MPa) Yield Strength |
| SAE AMS4970K | Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated |
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