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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Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
Available format(s)

PDF

Superseded date

14-05-2021

Language(s)

English

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
DevelopmentNote
Supersedes MIL HDBK 1587. (07/2017)
DocumentType
Standard
Pages
34
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
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 AMS 4990 : 2015 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 AMS 6906 : 2015 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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