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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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Superseded date
05-14-2021
Superseded by
Language(s)
English
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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Superseded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 AMS 6910 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 8AL - 1MO - 1V, DUPLEX ANNEALED |
| SAE AMS A 21180 : 2011 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| SAE AMS S 8802 : 2015 | SEALING COMPOUND, FUEL RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
| SAE AMS 6925 : 2015 | 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 AMS C 27725 : 2016 | COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES 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 AMS 6900 : 2015 | 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 AMS 4940 : 2012 | TITANIUM SHEET, STRIP, AND PLATE COMMERCIALLY PURE ANNEALED, 25.0 KSI (172 MPA) YIELD STRENGTH |
| SAE AMS 4915 : 2013 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1V - 1MO SINGLE ANNEALED |
| SAE AMS 6932 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V EXTRA LOW INTERSTITIAL, ANNEALED |
| SAE AMS 4911 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| SAE AS 81550A : 2014 | INSULATING COMPOUND, ELECTRICAL, EMBEDDING, REVERSION RESISTANT SILICONE |
| ASTM B 265 : 2015 : REDLINE | Standard Specification for Titanium and Titanium Alloy Strip, Sheet, and Plate |
| SAE AMS P 5510 : 2013 | O-RING, PREFORMED, STRAIGHT THREAD TUBE FITTING BOSS, TYPE 1 HYDRAULIC (-65 TO 160 DEGREES F) |
| SAE AMS 4989 : 2014 | 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 AMS R 83285 : 2011 | 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 AMS 2770 : 2015 | HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS |
| SAE AS 28775 : 2013 | 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 AS 3581 : 2012 | PACKING, PREFORMED - O-RING SEAL AMS 7259 |
| SAE AMS 4918 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 6921 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 7276H : 2011 | RUBBER: FLUOROCARBON (FKM) HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
| SAE AS 3208 : 1976 | 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 AMS 4919 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 6AL - 2SN - 4ZR - 2MO - 0.08SI DUPLEX ANNEALED |
| SAE AMS 6905 : 2014 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 2.0MO, DUPLEX ANNEALED |
| SAE AMS 3216 : 2005 | ELASTOMER: 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 AMS 4902 : 2013 | TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY-PURE, ANNEALED 40.0 KSI (276 MPA) YIELD STRENGTH |
| SAE AMS 3384 : 2013 | 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 AMS 6940 : 2011 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3.0AL - 2.5V, ANNEALED |
| SAE AMS A 22771 : 2012 | ALUMINUM ALLOY FORGINGS, HEAT TREATED |
| JSSG-2010 Base Document:1998 | Crew Systems |
| SAE AMS 2759 : 2014 | HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS |
| AWS C3.5M/C3.5 : 2016 | SPECIFICATION FOR INDUCTION BRAZING |
| SAE AMS 2301 : 2015 | STEEL CLEANLINESS, AIRCRAFT QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE |
| SAE AMS P 83461 : 1998 | Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C) |
| SAE AS 568 : 2014 | 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 AMS 2430 : 2015 | SHOT PEENING |
| SAE AMS 6907 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, DUPLEX ANNEALED |
| SAE AMS 6915 : 2015 | 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 AMS 4917 : 2012 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11CR - 3.0AL - SOLUTION HEAT TREATED |
| SAE AMS 6931 : 2014 | 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 AS 1933 : 2013 | AGE CONTROLS FOR HOSE CONTAINING AGE-SENSITIVE ELASTOMERIC MATERIAL |
| SAE AMS QQ A 367 : 2012 | ALUMINUM ALLOY FORGINGS |
| SAE AMS 2750 : 2012 | PYROMETRY |
| MIL R 25988/3 : 0 | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, O-RINGS, CLASS 1, GRADE 60 |
| SAE AMS 6926 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 7287 : 2012 | FLUOROCARBON ELASTOMER (FKM) HIGH TEMPERATURE/HTS OIL RESISTANT/FUEL RESISTANT LOW COMPRESSION SET/70 TO 80 HARDNESS, LOW TEMPERATURE TG -22 DEGREES F (-30 DEGREES C) FOR SEALS IN OIL/FUEL/SPECIFIC HYDRAULIC SYSTEMS |
| SAE AS 83461/2 : 2016 | STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 RUBBER |
| SAE AMS 6920 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
| SAE AMS 3100 : 2013 | ADHESION PROMOTER FOR POLYSULFIDE SEALING COMPOUNDS |
| SAE AMS R 7362 : 2012 | NITRILE RUBBER, SYNTHETIC, SOLID, SHEET, STRIP AND FABRICATED PARTS, SYNTHETIC OIL RESISTANT |
| SAE ARP 5316 : 2014 | STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
| SAE AMS 7259 : 2013 | RUBBER: FLOUROCARBON (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 AMS 4910 : 2017 | 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 AMS 4907 : 2013 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6.0AL - 4.0V, EXTRA LOW INTERSTITIAL, ANNEALED |
| SAE AMS 2772 : 2016 | 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 AMS 2303 : 2016 | 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 AMS 4921 : 2016 | TITANIUM BARS, WIRE, FORGINGS, AND RINGS COMMERCIALLY PURE, 70 KSI (483 MPA) YIELD STRENGTH |
| SAE AMS 4988 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED |
| FED-STD-191 Revision A:1978 | TEXTILE TEST METHODS |
| SAE AMS H 81200 : 2014 | HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS |
| SAE AMS 3218 : 2005 | ELASTOMER: FLUOROCARBON (FKM) RUBBER HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET 85 TO 95 |
| SAE AS 83461/1 : 2016 | M83461 O-RING MOLDED FROM AMS-P-83461 RUBBER |
| SAE AS 29561 : 2015 | O-RING, SYNTHETIC LUBRICANT RESISTANT MOLDED FROM AMS-R-7362 RUBBER |
| SAE AS 28778 : 2016 | O-RING, STRAIGHT THREAD TUBE FITTING BOSS MOLDED FROM AMS-P-5510 RUBBER |
| SAE AMS 4904 : 2015 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4909 : 2016 | 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 AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
| 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) |
| SAE AMS F 7190 : 2016 | 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 AMS 4903 : 2015 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED |
| SAE AMS 2300 L : 2015 | STEEL CLEANLINESS, PREMIUM AIRCRAFT-QUALITY MAGNETIC PARTICLE INSPECTION PROCEDURE |
| SAE AMS 3856 : 2016 | CLOTH, UPHOLSTERY, FLAME RESISTANT |
| SAE AMS 6930 : 2014 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4916 : 2014 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| SAE AS 3209 : 2013 | PACKING, PREFORMED - AMS 7276, 'O' RING |
| SAE AMS P 5315 : 2013 | 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 AMS 6936 : 2015 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 6935 : 2015 | 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 AMS 6901 : 2015 | 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 AMS 4901 : 2015 | 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 AMS 4900 : 2014 | TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 55.0 KSI (379 MPA) YIELD STRENGTH |
| SAE AMS 4970 : 2016 | TITANIUM ALLOY BARS, WIRE, AND FORGINGS 7AL - 4MO SOLUTION AND PRECIPITATION HEAT TREATED |
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