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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587)
Available format(s)
PDF
Published date
18-07-1996
Publisher
Superseded date
21-06-2017
Superseded by
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Establishes requirements for materials and processes used during design and production of aerospace weapon systems.
| DevelopmentNote |
NOTICE 1 - Notice of Cancellation/Superseded by MIL STD 1587. (07/2017)
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| DocumentType |
Standard
|
| Pages |
37
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy |
This standard establishes the requirements for materials and processes used during design and production of aerospace weapons systems. When used in conjunction with Mil-Std-1530, the other integrity program documents (Mil-Std-1783, Mil-Std-1798, etc.) and Mil-Std-1568, it is expected that structurally reliable aerospace systems having a good balance between acquisition costs and life cycle costs will result.
| MIL-STD-186 Revision F:2002 | Manufacturing Process Protective Finishingfor Army Missile Weapon Systems |
| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| SAE AS4073A | 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 (S/S by SAE-AS81550) |
| MIL-R-83248 Revision C:1994 | RUBBER, FLUOROCARBON ELASTOMER, HIGH TEMPERATURE, FLUID, AND COMPRESSION SET RESISTANT (S/S BY SAE-AMS7276, SAE-AMS7259, SAE-AMS3216, AND SAE-AMS3218) |
| MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
| MIL-M-24041 Revision C:1981 | Molding and Potting Compound, Chemically Cured, Polyurethane |
| MIL-S-9041 Revision B:1975 | Sandwich Construction; Plastic Resin, Glass Fabric Base, Laminated Facings and Honeycomb Core for Aircraft Structural and Electronic Applications |
| ASTM E 1 : 2014 : REDLINE | Standard Specification for ASTM Liquid-in-Glass Thermometers |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-A-46146 Revision B:1990 | Adhesives-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 (S/S BY SAE-AMS-P-5315) |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF (NO S/S DOCUMENT) |
| MIL-A-83377 Revision B:1978 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for (No S/S Document) |
| 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 (S/S BY SAE-AMS-R-83485) |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AMS2770M | Heat Treatment of Wrought Aluminum Alloy Parts |
| MIL-T-81556 Revision A:1983 | Titanium and Titanium Alloys, Extruded Bars and Shapes, Aircraft Quality |
| MIL-A-22771 Revision D:1984 | Aluminum Alloy Forgings, Heat Treated (S/S by SAE-AMS-A-22771) |
| MIL R 6855 : E | RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES |
| MIL-STD-1783 Base Document:1984 | ENGINE STRUCTURAL INTEGRITY PROGRAM (ENSIP) (S/S BY MIL-HDBK-1783) |
| 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 (S/S by SAE-AMS-C-27725) |
| MIL-S-8802 Revision F:1990 | SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH-ADHESION (S/S BY SAE-AMS-S-8802) |
| QQ-A-367 Revision H:1973 | Aluminum Alloy Forgings (S/S by SAE-AMS-QQ-A-367) |
| SAE AMS2759E | Heat Treatment of Steel Parts General Requirements |
| SAE AMS2301K | Steel Cleanliness, Aircraft Quality Magnetic Particle Inspection Procedure |
| SAE AS568D | Aerospace Size Standard for O-rings |
| MIL-T-9046 Revision J:1983 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE (S/S BY SAE-AMS-T-9046) |
| MIL-STD-2175 Revision A:1993 | CASTINGS, CLASSIFICATION AND INSPECTION OF (S/S BY SAE-AMS-STD-2175) |
| MS29513 Revision C:1966 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, \"O\" RING (S/S BY SAE-AS29513) |
| MIL-E-47231 Base Document:1974 | Electrical Components, Potting of (No S/S Document) |
| 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 | Galvanic Compatibility of Electrically Conductive Materials |
| 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 (See Notice 1 for Replacement Information) |
| 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 (S/S BY SAE-AS28778) |
| MS28775 Revision E:1984 | PACKING, PREFORMED, HYDRAULIC, +275 DEG. F (\"O\" RING) (S/S BY SAE-AS28775) |
| SAE AMS2750E | 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, \"O\" RING (S/S BY SAE-AS29512) |
| MIL-F-7190 Revision B:1985 | Forging, Steel, for Aircraft/Aerospace Equipment and Special Ordinance Applications (S/S by SAE-AMS-F-7190) |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL-STD-1595 Revision A:1982 | QUALIFICATION OF AIRCRAFT, MISSILE & AEROSPACE FUSION WELDERS (SAE-AMS-STD-1595) |
| SAE AMS3100D | 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 (S/S by AWS-D17.1) |
| 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 (NO S/S DOCUMENT) |
| SAE AMS2303F | 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 (Future Acquisition should specify one AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7) |
| MIL-STD-1523 Revision A:1984 | AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIEL (FOR AEROSPACE APPLICATIONS) (S/S BY SAE-AS1933 AND SAE-ARP5316) |
| 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 (S/S by SAE-AMS-A-21180) |
| 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 (NO S/S DOCUMENT) |
| 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) |
| MIL-H-6088 Revision G:1991 | Heat Treatment of Aluminum Alloys (S/S by SAE-AMS-H-6088) |
| MS29561 Revision A:1966 | PACKING, PREFORMED, O RING, SYNTHETIC LUBRICANT RESISTANT (S/S BY SAE-AS29561) |
| MIL-W-6858 Revision D:1978 | WELDING, RESISTANCE: SPOT AND SEAM (S/S BY SAE-AMS-W-6858) |
| SAE AMS2300L | Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure |
| SAE AMS3856B | Cloth, Upholstery, Flame Resistant |
| MIL-P-83461 Revision B:1980 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEG. F (135 DEG. C) (S/S BY SAE-AMS-P-83461) |
| MIL-I-16923 Revision H:1991 | Insulating Compound, Electrical, Embedding, Epoxy (S/S by A-A-59877) |
| ZZ-R-765 Revision E:1991 | RUBBER, SILICONE (GENERAL SPECIFICATION) (S/S BY A-A-59588) |
| 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 (See Notice 2 for Replacement Information) |
| MIL-F-83142 Revision A:1969 | Forging, Titanium Alloys, Premium Quality (See Notice 5 for Replacement Information) |
| 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 AT 275 DEGREE F (135 DEGREE C) SIZES AND TOLERANCES (S/S BY SAE-AMS-P-83461/1) |
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