MIL-H-6875 Revision H:1989
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875)
Available format(s)
PDF
Published date
03-01-1989
Publisher
Superseded date
02-02-1999
Superseded by
US$20.00
Excluding Tax where applicable
NO CONTENTS SECTION
Describes heat-treatment of four classes of steel.
| DevelopmentNote |
MIL-H-6875 H NOTICE 1 - NOTICE OF CANCELLATION FUTURE ACQUISITIONS FOR THIS ITEM SHOULD REFER TO SAE-AMS-H-6875, "HEAT TREATMENT OF STEEL RAW MATERIALS"
|
| DocumentType |
Standard
|
| Pages |
35
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| SAE AMS2759/6B | Similar to |
| SAE AMS2759E | Similar to |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-STD-2156 Base Document:1983 | Launcher, Rail, Guided Missile, Aircraft, General Design Criteria for |
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| MIL-S-5944 Revision C:1990 | SLINGS, AIRCRAFT, GENERAL SPECIFICATION FOR (S/S BY SAE-AS5944) |
| MIL-J-26149 Revision E:1988 | Jack, Hydraulic, Aircraft Maintenance, General Specification for |
| API 16C RUSSIAN : 1993 | SPECIFICATION FOR CHOKE AND KILL SYSTEMS |
| MIL-A-83577 Revision B:1988 | Assemblies, Moving Mechanical, for Space and Launch Vehicles, General Specification for (No S/S Document) |
| DIN 65570:1990-12 | AEROSPACE; HEAT TREATMENT FACILITIES; GENERAL REQUIREMENTS |
| MIL-W-63071 Revision A:1980 | Warhead, for Demolition Kit, M180 Metal Parts for |
| MIL P 60547 : F | PROJECTILE, 105 MM, HE, M1 & M760 METAL PARTS ASSEMBLY |
| MIL-M-8555 Revision C:1984 | Missile, Guided, Design and Construction, General Specification for (No S/S Document) |
| MS22046 Revision C:1974 | RING-PARACHUTE HARNESS \"D\" (S/S BY PIA-PS22046) |
| MIL S 81081 : A | STEEL; SHEET, CHROMIUM NICKEL MOLYBDENUM VANADIUM (FOR TORPEDO MARK 46 MOD O) |
| MIL P 45952 : 0 | PIN,QUICK RELEASE, DETENT GENERAL SPECIFICATION FOR |
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| MIL-S-45933 Base Document:1971 | STUD, KEYRING LOCKED, 125 AND 160 KSI FTU, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL-D-70789 Revision A:1992 | Dynamic Reference Unit (DRU) |
| MIL-STD-1881 Base Document:1983 | BRAZING SILVER, GENERAL PROCESS FOR (NO S/S DOCUMENT) |
| MIL-G-16959 Revision B:1967 | Gaskets; Metallic, Boiler, Economizer and Superheater Handhole |
| MIL-STD-1892 Base Document:1985 | WELDING, ARC AND OXYFUEL GAS, PROCESS AND REQUIREMENTS FOR (NO S/S DOCUMENT) |
| MIL-W-8611 Revision A:1957 | WELDING, METAL ARC AND GAS, STEELS, AND CORROSION AND HEAT RESISTANT ALLOYS; PROCESS FOR (S/S BY MIL-STD-2219) |
| MS70108 Revision C:1986 | LINK, PARACHUTE CONNECTOR (S/S BY PIA-PS70108) |
| MIL T 8878 : D | TURNBUCKLE, POSITIVE SAFETYING |
| MIL R 007885 : C SUPP 1 | RIVETS; BLIND, STRUCTURAL, LOCKED AND FRICTION RETAINED SPINDLE, GENERAL SPECIFICATION FOR |
| MIL-S-8844 Revision D:1987 | STEEL BAR, REFORGING STOCK, AND MECHANICAL TUBING, LOW ALLOY, PREMIUM QUALITY (S/S BY SAE-AMS6414 AND SAE-AMS6257) |
| MIL-P-48094 Revision B:1981 | PROJECTILE, 8 INCH, HE, M509A1 HARDWARE NON METALLIC (NO S/S DOCUMENT) |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) (NO S/S DOCUMENT) |
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| SAE AS5944 | Slings, Aircraft, General Specification For |
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| MIL-P-5673 Revision D:1983 | PIN, STRAIGHT, HEADED (S/S BY NASM5673) |
| MIL-B-8907 Revision A:1983 | Bolt, Alloy Steel, Shear and Tensile (156 KSI FSU and 260 KSI FTU, 450 Degrees F) External Wrenching, Flanged Head (S/S by NASM8907) |
| MIL-P-23460 Revision E:1991 | PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING (S/S BY NASM23460) |
| MIL-B-87114 Revision A:1978 | BOLTS, RECESS DRIVE, GENERAL SPECIFICATION FOR |
| MS17988 Revision E:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, DOUBLE ACTING, \"T\" HANDLE (S/S BY NASM17988) |
| MIL-B-8906 Revision C:1988 | Bolt, Alloy Steel, Shear and Tensile, (132 KSI FSU and 220 KSI FTU), 450 Degrees F, Spline Drive, General Specification for (S/S by NASM8906) |
| MIL-S-21472 Revision C:1988 | SCREW, SHOULDER, HEXAGON SOCKET-HEAD AND SLOTTED-HEAD GENERAL SPECIFICATION FOR (S/S BY NASM21472) |
| MIL-S-45909 Revision C:1989 | STUD, LOCKED IN, RING LOCKED, SERRATED, GENERAL SPECIFICATION FOR (S/S BY NASM45909) |
| MIL-B-23964 Revision D:1981 | Bolt, Self-Retaining, Positive Locking (S/S by NASM23964) |
| MIL-F-81177 Revision E:1984 | Fastener, Blind, High Strength, Installation Formed, Alloy Steel, General Specification for (S/S by NASM81177) |
| MS17987 Revision G:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, RING HANDLE (S/S BY NASM17987) |
| MIL-F-22978 Revision A:1963 | Fastener, Rotary, Quick-Operating, High-Strength (ASG) (S/S by NASM22978) |
| MIL-A-81973 Base Document:1974 | Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document) |
| MIL-B-83050 Revision D:1985 | Bolt, Self-Retaining, Impedance Type (S/S by NASM83050) |
| MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT (S/S BY NASM7839) |
| MIL-B-85604 Revision A:1988 | BOLT, NICKEL ALLOY 718, TENSION, HIGH STRENGTH, (125 KSI FSU & 220 KSI FTU) HIGH TEMPERATURE, SPLINE DRIVE, GENERAL SPECIFICATION FOR |
| MIL-T-81364 Base Document:1966 | T-BOLT, 180,000 PSI, TYPE 431 STAINLESS STEEL, MANUFACTURING PROCESS REQUIREMENTS (NO S/S DOCUMENT) |
| DOD-STD-1312-111 Base Document:1984 | FASTENER TEST METHODS, METRIC METHOD 111 TENSION FATIGUE (S/S BY NAM1312-111) |
| MIL-N-85730 Base Document:1988 | NUT, SELF-LOCKING, SPLINE DRIVE, ASSEMBLED WASHER, NICKEL ALLOY 718, 220 KSI FTU, 900 DEGREES F, GENERAL SPECIFICATION FOR |
| MIL-STD-1312-11 Revision A:1984 | FASTENER TEST METHODS METHOD 11, TENSION FATIGUE (S/S BY NASM1312-11) |
| MIL-B-8831 Revision B:1982 | Bolt, 180 KSI FTU and 180 KSI FSU, 450 Degrees F Protruding and Flush Head, General Specification for (S/S by NASM8831) |
| MIL-K-27545 Revision B:1989 | Key, Woodruff, Alloy Steel (S/S by NASM27545) |
| MIL-B-7838 Revision C:1989 | Bolt, Internal Wrenching, 160 KSI FTU (S/S by NASM7838) |
| MS17984 Revision F:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, BUTTON HANDLE (S/S BY NASM17984) |
| MS17986 Revision G:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, \"L\" HANDLE (S/S BY NASM17986) |
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| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-B-85464 Base Document:1981 | BOOSTER, FUSE, MARK 38 MOD 2 |
| MIL-S-6090 Revision A:1971 | STEELS USED IN AIRCRAFT CARBURIZING AND NITRIDING, PROCESS FOR (S/S BY SAE-AMS-S-6090) |
| MIL-STD-1876 Revision A:1991 | Nitriding, Gaseous Atmosphere Processing for (No S/S Document) |
| SAE AS4444 | Fittings, 24° Cone Flareless, Fluid Connection, 5000 psi |
| MIL-I-45934 Base Document:1971 | Insert, Screw Thread, Keyring Locked, Self Locking and Non Self Locking, 125, 180, and 220 KSI FTU: General Specification for (No S/S Document) |
| MIL P 14852 : B | PROJECTILE, 105 MM ILLUMINATING, M314A3, METAL PARTS ASSEMBLY |
| MIL-E-50796 Base Document:1973 | Expanding Shielded Mild Detonating Cord Assembly |
| MIL C 6458 : C | CHAIN ASSEMBLY, SINGLE LEG, AIRCRAFT CARGO TIE DOWN |
| MIL-S-8967 Base Document:1968 | STEEL BARS, WIRE, FORGING STOCK, FORGINGS, MECHANICAL TUBING, (431) PREMIUM QUALITY (NO S/S DOCUMENT) |
| MIL-R-43003 Revision F:1994 | Release, Cargo Parachute, 5000-Pound Capacity |
| MIL-A-83469 Base Document:1976 | Adjuster, Lap Belt, 1-3/4 Inch Webbing (No S/S Document) |
| MIL-S-8512 Revision D:1974 | Support Equipment, Aeronautical, Special, General Specification for the Design of |
| MIL L 38671 : A | LUG, SUSPENSION, BOMB MAU-129/A, "T" TYPE |
| MIL-STD-2131 Revision A:1991 | Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for |
| SAE MA2060A | Fittings, Welded, Hydraulic, Titanium and Corrosion Resistant Steel, 21 000 kPa, Metric |
| MIL R 46963 : A | ROCKET MOTOR, M42A1, BOOSTER |
| MIL-DTL-85110 Revision B:1997 | Bar, Repeatable Release Holdback (RRHB), Aircraft Launching, General Requirement for |
| ISO 10433:1994 | Petroleum and natural gas industries — Drilling and production equipment — Specification for wellhead surface safety valves and underwater safety valves for offshore service |
| API 7NRV : 2006 : R2012 | SPECIFICATION FOR DRILL STRING NON-RETURN VALVES |
| SAE AMS5340E | Steel, Corrosion Resistant, Investment Castings 14Cr - 4.25Ni - 2.25Mo - 0.25Cb - 3.25Cu Homogenization and Solution Heat Treated |
| SAE AMSF7190B | Forging, Steel, For Aircraft/Aerospace Equipment and Special Ordnance Applications |
| MIL-K-8662 Revision E:1974 | Knife, Hunting, Sheathed, Survival, Pilot\'s (S/S by SAE-AS8662) |
| TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| SAE MAM6415C | Steel, Bars, Forgings, and Tubing, 0.80cr 1.8ni 0.25mo (0.38 0.43) |
| MIL-F-85731 Base Document:1986 | Fastener, Positive Locking, Electronic Equipment General Specificationfor |
| MIL-P-63226 Base Document:1979 | Projectile, Guided, 155mm, XM712, Warhead For |
| MIL-Q-22631 Revision B:1964 | Quality Control of Metal Wrought Products Except Forgings Procured to Non-Governmental Specification (No S/S Document) |
| MIL-T-8606 Revision C:1973 | Tubing, Steel, Corrosion-Resistant (18-8 Stabilized and Extra Low Carbon) (Use SAE-AMS5560, SAE-AMS5563, SAE-AMS5564, SAE-AMS5565, SAE-AMS5566, SAE-AMS5567, SAE-AMS5569, SAE-AMS5570, SAE-AMS5571, SAE-AMS5639 and SAE-AMS5668) |
| MIL-STD-1547 Revision B:1992 | Electronic Parts, Materials, and Processes for Space and Launch Vehicles |
| MIL-F-80233 Revision B:1985 | Furnace, Vacuum, Heat Treating, Integral Quench (No S/S Document) |
| MIL-B-9972 Revision B:1994 | Brazing, Nickel Alloy, General Specification for (S/S by AWS-C3.6) |
| MIL-F-5509 Revision D:1978 | Fitting, Flared Tube, Fluid Connection (see Notice 2 for Additional Superseding Information) |
| SAE MA2150 | Clamps, Loop or P Style, Single Point Mount, Multiple Shapes, Metric |
| MIL-I-45914 Revision A:1991 | Insert, Screw Thread - Locked in, Key Locked, General Specification for |
| MS70101 Revision C:1986 | ADAPTER, REVERSIBLE, QUICK FIT, 500 LBS 1-3/4 INCH (S/S BY PS70101) |
| SAE AMS5348C | Steel Castings, Tubular, Centrifugal, Corrosion Resistant 15Cr - 4.6Ni - 0.22 (Cb+Ta) - 2.8Cu Solution Heat Treated |
| MIL-S-81591 Base Document:1968 | Steel, Investment Castings, Carbon and Corrosion Resisting |
| MIL S 25073 : 0 | |
| DOD-S-63543 Base Document:1982 | Stud and Rod, Threaded, Metric, General Specification for (No S/S Document) |
| MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION (S/S BY SAE-AMS-T-6845) |
| SAE AMSQQS763D | Steel, Corrosion Resistant, Bars, Wire, Shapes, and Forgings |
| SAE AS4510 | Fittings, Weld, Fluid Connection, 5000 psi |
| SAE AS8662 | Knife, Hunting, Sheathed, Survival, Pilot’s |
| SAE AMS5341D | Steel Castings, Investment, Corrosion Resistant 19.5Cr - 10.5Ni - 0.25S (Type 303) Solution Heat Treated |
| BS EN ISO 14693:2003 | Petroleum and natural gas industries. Drilling and well-servicing equipment |
| API 7K : 2015 INC ERR 2:2016 | DRILLING AND WELL SERVICING EQUIPMENT |
| MIL-G-48047 Revision B:1981 | Grenade, GP, M46 Body Assembly, Type CA, for |
| MIL-R-5632 Revision B:1972 | RODS AND WIRE, STEEL, WELDING (FOR AIRCRAFT APPLICATIONS) (S/S BY SAE-AMS6457, SAE-AMS6452, SAE-AMS6456, SAE-AMS6459, SAE-AMS6331, SAE-AMS6461, SAE-AMS6462, SAE-AMS6458, SAE-AMS5027 AND SAE-AMS5028) |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| FF-S-210 Revision B:1981 | Setscrews: Square Head (Inch) and Slotted Headless (Inch and Metric) |
| MIL C 83438 : 1986 | CLOTHING OUTFITS, EXTREME COLD WEATHER SURVIVAL |
| API 8C : 2012 | DRILLING AND PRODUCTION HOISTING EQUIPMENT (PSL 1 AND PSL 2) |
| SAE AMS5384F | Alloy Castings, Investment, Corrosion and Heat Resistant 53Ni - 18Cr - 18Co - 4.0Mo - 2.9Ti - 2.9Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution and Precipitation Heat Treated |
| DOD-S-63275 Revision A:1982 | Stud, Screw Thread, Locked in, Ring Locked, Serrated, Metric and Ring, Lock, Serrated, Metric, General Specification for (No S/S Document) |
| MIL S 9479 : C | |
| MIL-R-43838 Revision B:1993 | RELEASE, CARGO PARACHUTE, AIRDROP, M-2 (FUTURE ACQUISITION USE DRAWING 11-1-565) |
| MIL-B-22036 Revision D:1991 | Bridle and Pendant Assemblies Aircraft Launching |
| MIL-C-43899 Revision A:1985 | Coupling, Extraction Force Transfer, Platform (No S/S Document) |
| MIL-HDBK-506 Base Document:1998 | Process for Coating, Pack Cementation, Chrome Aluminide |
| MIL-F-13926 Revision B:1984 | Fire Control Materiel, Manufacture and Inspection, General Specification for |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-N-85729 Base Document:1988 | NUT, SELF-LOCKING, A-286, 160 KSI FTU, 450 DEGREES F, GENERAL SPECIFICATION FOR |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-R-7885 Revision D:1988 | Rivets, Blind, Structural, Mechanically LockedSpindleand Friction Locked Spindle, General Specification for |
| MIL-STD-340 Base Document:1988 | COATING, PACK CEMENTATION, CHROME ALUMINIDE, PROCESS FOR (S/S BY MIL-HDBK-506) |
| MIL-A-23899 Revision B:1984 | Aural Protector, Sound (S/S by SAE-AS23899) |
| SAE MA2100 | Hose Assemblies, Metal Medium Pressure, High Temperature, Metric |
| API 11V1 :1995 | SPECIFICATION FOR GAS LIFT EQUIPMENT |
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| SAE AMS5330E | Steel Castings, Investment 0.80Cr - 1.8Ni - 0.35Mo (0.38 - 0.46C) (SAE 4340 Modified) Annealed |
| API 7K CHINESE : 2010 | DRILLING AND WELL SERVICING EQUIPMENT |
| ISO 14693:2003 | Petroleum and natural gas industries — Drilling and well-servicing equipment |
| EN ISO 14693:2003 | Petroleum and natural gas industries - Drilling and well-servicing equipment (ISO 14693:2003) |
| MIL-H-7195 Revision G:1991 | Hardware, Parachute, General Specification for (S/S by PIA-H-7195) |
| MIL-R-81294 Revision D:1990 | Remover, Paint, Epoxy, Polysulfide, and Polyurethane Systems |
| MIL-H-47143 Base Document:1974 | Heat Treating, Type D6AC Alloy Steel, Processes for (No S/S Document) |
| MIL-T-8506 Revision A:1966 | TUBING, STEEL, CORROSION-RESISTANT, (304) ANNEALED, SEAMLESS AND WELDED (S/S BY SAE-AMS-T-8506) |
| SAE AMS5363F | Steel Castings, Sand and Centrifugal, Corrosion and Heat Resistant 18.5Cr - 10.5Ni - 0.90 (Cb+Ta) Solution Heat Treated |
| MIL-S-23008 Revision D:1988 | Steel Castings, Alloy, High Yield Strength (HY-80 and HY-100) (See Notice 2 for Replacement Information) |
| MIL-STD-1877 Revision B:1990 | BRAZING, NICKEL, HIGH TEMPERATURE VACUUM (METRIC) (NO S/S DOCUMENT) |
| MIL-S-24512 Base Document:1975 | Steel Forgings, Alloy, Structural, High Yield Strength (HY-130) (See Notice 3 for Replacement Information) |
| SAE AS 85075 : 2000 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
| MIL-R-46509 Revision A:1982 | ROCKET MOTOR, M30, METAL PARTS FOR (NO S/S DOCUMENT) |
| MIL-B-85107 Revision B:1988 | Bearing, Spin (Sidewinder) (No S/S Document) |
| QQ-S-763 Revision F:1996 | STEEL BARS, WIRE, SHAPES, AND FORGINGS; CORROSION RESISTANT (S/S BY SAE-AMS-QQ-S-763) |
| MIL-E-8697 Revision E:1972 | Electrodes, Welding, Covered, Low-Hydrogen, Heat-Treatable Steel (No S/S Document) |
| MIL-B-81936-1 Revision B:1994 | Bearing, Plain, Self-Aligning, BECU Ball, CRES Race, (with Stacking Groove) -65 Deg. F to +350 Deg. F (S/S by SAE-AS81936/1) |
| MIL-W-6873 Revision C:1991 | Welding; Flash, Carbon and Alloy Steel (See Notice 2 for Replacement Information) |
| MIL S 46188 : 0 | STEEL PLATE, WROUGHT HOMOGENEOUS ELECTROSLAG REMELT (ESR) (4340 ALLOY |
| MIL-C-83435 Base Document:1974 | Clothing Outfit, Extreme Cold Weather Survival A/P22S-10 (No S/S Document) |
| MIL-L-40085 Revision F:1989 | Link Assembly, Type IV, Air Delivery (No S/S Document) |
| NASA MSFC STD 506 : 1988 | MATERIALS AND PROCESSES CONTROL |
| MIL-F-7190 Revision B:1985 | Forging, Steel, for Aircraft/Aerospace Equipment and Special Ordinance Applications (S/S by SAE-AMS-F-7190) |
| NASA STD 6002 : 2008 | APPLYING DATA MATRIX IDENTIFICATION SYMBOLS ON AEROSPACE PARTS |
| MIL K 20277 : H | KNIFE, COMBAT AND SHEATH |
| MIL-S-18732 Revision D:1968 | Steel Bars, Wire, Forging Stock, Forgings Tubing (431), Special Quality |
| MIL S 81018/2 : D NOTICE 3 | SURVIVAL KIT CONTAINER, AIRCRAFT SEAT, WITH OXYGEN, RSSK-8D |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| MIL-STD-40002 Base Document:1991 | HEAT TREATMENT CODING SYSTEM, GENERAL (NO S/S DOCUMENT) |
| DOD STD 1312/11 : LATEST | FASTENER, TEST METHODS METRIC, METHOD 11, TENSION FATIGUE (S/S BY DOD STD 1312-111) |
| API 7NRV CHINESE : 2006 | SPECIFICATION FOR DRILL STRING NON-RETURN VALVES |
| SAE AS7101C | National Aerospace and Defense Contractors Accreditation Program (NADCAP) General Requirements for Materials Test Laboratory Accreditation Program |
| SAE AS23899A | Aural Protector, Sound |
| API 7K : 2015 | DRILLING AND WELL SERVICING EQUIPMENT |
| API 7K REDLINE : 2010 | DRILLING AND WELL SERVICING EQUIPMENT |
| ASTM A 262 : 2015 : REDLINE | Standard Practices for Detecting Susceptibility to Intergranular Attack in Austenitic Stainless Steels |
| ASTM E 384 : 2017 : REDLINE | Standard Test Method for Microindentation Hardness of Materials |
| SAE AMS2759/3F | Heat Treatment Precipitation-Hardening Corrosion-Resistant and Maraging Steel Parts |
| SAE AMS2418J | Plating, Copper |
| SAE AMS2759E | Heat Treatment of Steel Parts General Requirements |
| ASTM D 3520 : 2004 | Standard Test Method for Quenching Time of Heat-Treating Fluids (Magnetic Quenchometer Method) (Withdrawn 2008) |
| ASTM E 10 : 2017-05 | TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS |
| SAE AMS2750E | Pyrometry |
| MIL-C-14550 Revision B:1983 | Copper Plating (Electrodeposited) (S/S by SAE-AMS2418) |
| ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-N-290) |
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