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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 RAW MATERIALS
Available format(s)
PDF
Superseded date
02-02-1999
Publisher
NO CONTENTS SECTION
Describes heat-treatment of four classes of steel.
Committee |
FSC 95GP
|
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Superseded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 AMS H 6875 : 2010 | Similar to |
SAE AMS 2759/6 : 2005 | Similar to |
SAE AMS 2759 : 2014 | 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 |
API 16C CHINESE : 1993 | SPECIFICATION FOR CHOKE AND KILL SYSTEMS |
MIL-S-5944 Revision C:1990 | SLING, AIRCRAFT, GENERAL SPECIFICATION FOR |
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 |
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 |
MS22046 Revision C:1974 | RING - PARACHUTE HARNESS "D" |
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 |
MIL-W-83970 Revision B:1981 | WING AND ROLLERON ASSEMBLY AIM-9 |
AWS BRH:2007 | BRAZING HANDBOOK |
MIL-S-45933 Base Document:1971 | STUD, KEYRING LOCKED, 125 AND 160 KSI FTU, GENERAL SPECIFICATION FOR |
MIL-D-70789 Revision A:1992 | DYNAMIC REFERENCE UNIT (DRU) |
MIL-STD-1881 Base Document:1983 | BRAZING SILVER, GENERAL PROCESS FOR |
MIL-G-16959 Revision B:1967 | GASKET, METALLIC, BOILER, ECONOMIZER AND SUPERHEATER HANDHOLE |
MIL-STD-1892 Base Document:1985 | WELDING, ARC AND OXYFUEL GAS, PROCESS AND REQUIREMENTS FOR |
MIL-W-8611 Revision A:1957 | WELDING, METAL ARC AND GAS STEELS AND CORROSION AND HEAT RESISTANT ALLOYS PROCESS FOR |
MS70108 Revision C:1986 | LINK PARACHUTE CONNECTOR |
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 |
MIL-P-48094 Revision B:1981 | PROJECTILE, 8 INCH, HE, M509A1 HARDWARE NON-METALLIC |
DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
SAE AS 85731 : 2015 | FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
SAE MA 2151 : 2015 | CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE AMS S 6090 : 2006 | STEEL CARBURIZING AND NITRIDING, PROCESSES FOR |
SAE AS 5944 : 1999 | SLINGS, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
MIL-P-5673 Revision D:1983 | PIN, STRAIGHT HEADED |
MIL-B-8907 Revision A:1983 | BOLT, ALLOY STEEL, SHEAR AND TENSILE (156 KSI FSU AND 260 KSI FTU, 450 DEGREE F) EXTERNAL WRENCHING, FLANGED HEAD |
MIL-P-23460 Revision E:1991 | PIN, QUICK-RELEASE, SELF-RETAINING POSITIVE-LOCKING |
MIL-B-87114 Revision A:1978 | BOLTS, RECESS DRIVE, GENERAL SPECIFICATION FOR |
MS17988 Revision E:1994 | PIN QUICK RELEASE POSITIVE LOCKING DOUBLE ACTING T HANDLE |
MIL-B-8906 Revision C:1988 | BOLT, ALLOY STEEL, SHEAR AND TENSILE, (132 KSI MIN FSU AND 220 KS MIN FTU), 45 DEGREE F, SPLINE DRIVE |
MIL-S-21472 Revision C:1988 | SCREW, SHOULDER, HEXAGON SOCKET-HEAD AND SLOTTED-HEAD GENERAL SPECIFICATION FOR |
MIL-S-45909 Revision C:1989 | STUD, LOCKED IN - RING LOCKED SERRATED |
MIL-B-23964 Revision D:1981 | BOLT, SELF-RETAINING, POSITIVE LOCKING |
MIL-F-81177 Revision E:1984 | FASTENERS, BLIND, HIGH STRENGTH, INSTALLATION FORMED ALLOY STEEL, GENERAL SPECIFICATION FOR |
MS17987 Revision G:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, RING HANDLE |
MIL-F-22978 Revision A:1963 | FASTENER, ROTARY, QUICK-OPERATING, HIGH STRENGTH (ASG) |
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 |
MIL-B-83050 Revision D:1985 | BOLT, SELF RETAINING, IMPEDANCE TYPE |
MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT |
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 |
DOD-STD-1312-111 Base Document:1984 | FASTENER TEST METHODS, METRIC METHOD 111, TENSION FATIGUE |
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 AND FATIGUE |
MIL-B-8831 Revision B:1982 | BOLT, 180 KSI FTU AND 180 KSI FSU 450 DEG F PROTRUDING AND FLUSH HEAD, GENERAL SPECIFICATION FOR |
MIL-K-27545 Revision B:1989 | KEY, WOODRUFF, ALLOY STEEL |
MIL-B-7838 Revision C:1989 | BOLT, INTERNAL WRENCHING 160 KSI FTU |
MS17984 Revision F:1994 | PIN QUICK RELEASE, SELF RETAINING POSITIVE LOCKING SINGLE ACTING BUTTON HANDLE |
MS17986 Revision G:1994 | PIN, QUICK RELEASE, SELF-RETAINING, POSITIVE LOCKING, SINGLE ACTING, "L" HANDLE |
MS21025 Revision F:1996 | NUT, CASTELLATED, HEXAGON |
MIL-B-45908 Revision B:1985 | BOLT, EYE, GENERAL SPECIFICATION FOR |
MIL-S-45915 Revision A:1967 | STUD, LOCKED IN - KEY LOCKED - GENERAL SPECIFICATION FOR |
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 | STEEL, CARBURIZING AND NITRIDING, PROCESSES FOR |
MIL-STD-1876 Revision A:1991 | NITRIDING, GASEOUS ATMOSPHERE PROCESSING FOR |
SAE AS 4444 : 2013 | FITTINGS, 24 DEGREE 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 |
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 BAR, WIRE, FORGING STOCK, FORGINGS, MECHANICAL TUBING [431] QUALITY |
MIL-R-43003 Revision F:1994 | RELEASE, CARGO PARACHUTE, 5,000 POUND CAPACITY |
MIL-A-83469 Base Document:1976 | ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
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 MA 2060 : 2015 | 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 |
NASM 7838 : 2004 | BOLT, INTERNAL WRENCHING, 160 KSI FTU |
NASM24694:2012 | SCREW, MACHINE, FLAT COUNTERSUNK HEAD, 100 DEGREES, STRUCTURAL, CROSS RECESSED, UNC-3A AND UNF-3A |
API 7NRV : 2006 : R2012 | SPECIFICATION FOR DRILL STRING NON-RETURN VALVES |
SAE AMS 5340 : 2018 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 14CR - 4.25NI - 2.25MO - 0.25CB - 3.25CU, HOMOGENIZATION AND SOLUTION HEAT TREATED |
SAE AMS F 7190 : 2016 | FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
MIL-K-8662 Revision E:1974 | KNIFE, HUNTING, SHEATHED, SURVIVAL PILOT S |
TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
NASM 23460 : 2004 | PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING |
MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
SAE MAM 6415 : 1998 | STEEL, BARS, FORGINGS, AND TUBING, 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
MIL-F-85731 Base Document:1986 | FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
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 SPECIFICATIONS |
MIL-T-8606 Revision C:1973 | TUBING, STEEL, CORROSION RESISTANT (18-8 STABILIZED AND EXTRA LOW CARBON) |
MIL-STD-1547 Revision B:1992 | ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES |
MIL-F-80233 Revision B:1985 | FURNACES, VACUUM, HEAT TREATING INTEGRAL QUENCH |
MIL-B-9972 Revision B:1994 | BRAZING, NICKEL, ALLOY, GENERAL SPECIFICATION FOR |
MIL-F-5509 Revision D:1978 | FITTING, FLARED TUBE, FLUID CONNECTION |
SAE MA 2150 : 2015 | CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC |
MIL-I-45914 Revision A:1991 | INSERT, SCREW THREAD - LOCKED IN, KEY LOCKED |
MS70101 Revision C:1986 | |
SAE AMS 5348 : 2017 | 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 & ROD, THREADED, METRIC, GENERAL SPECIFICATION FOR |
API 14D : 1994 | SPECIFICATION FOR WELLHEAD SURFACE SAFETY VALVES AND UNDERWATER SAFETY VALVES FOR OFFSHORE SERVICE |
MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION |
SAE AMS QQ S 763D : 2013(S2015) | STEEL, CORROSION RESISTANT, BARS, WIRE, SHAPES, AND FORGINGS |
SAE AS 4510 : 2013 | FITTINGS, WELD, FLUID CONNECTION, 5000 PSI |
SAE AS 8662 : 1999 | KNIFE, HUNTING, SHEATHED, SURVIVAL, PILOTS |
SAE AMS5341:2012(S2017) | 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+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 | ROD, AND WIRE, STEEL WELDING [FOR AIRCRAFT] |
NAS496:2002 | BOLTS - INTERNAL WRENCHING |
JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - 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 AMS 5384 : 2017 | 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 |
MIL S 9479 : C | |
MIL-R-43838 Revision B:1993 | RELEASE, CARGO PARACHUTE, AIRDROP, M-2 |
MIL-B-22036 Revision D:1991 | BRIDLE AND PENDANT ASSEMBLIES, AIRCRAFT LAUNCHING |
MIL-C-43899 Revision A:1985 | COUPLING, EXTRACTION FORCE TRANSFER, PLATFORM |
MIL-HDBK-506 Base Document:1998 | PROCESS FOR COATING, PACK CEMENTATION, CHROME ALUMINIDE |
MIL-F-13926 Revision B:1984 | FIRE CONTROL MATERIAL 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 | RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED SPINDLE AND FRICTION LOCKED SPINDLE, GENERAL SPECIFICATION FOR |
MIL-STD-340 Base Document:1988 | COATING, PACK CEMENTATION, CHROME ALUMINIDE, PROCESS FOR |
MIL-A-23899 Revision B:1984 | AURAL PROTECTOR, SOUND |
SAE MA 2100 : 2015 | HOSE ASSEMBLIES, METAL MEDIUM PRESSURE, HIGH TEMPERATURE, METRIC |
API 11V1 :1995 | SPECIFICATION FOR GAS LIFT EQUIPMENT |
API 7NRV : 2006 | SPECIFICATION FOR DRILL STRING NON-RETURN VALVES |
API 11V1 : 1995 : R2008 | SPECIFICATION FOR GAS LIFT EQUIPMENT |
SAE AMS 5330 : 2015 | 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 |
MIL-R-81294 Revision D:1990 | REMOVER, PAINT, EPOXY, POLYSULPHIDE AND POLYURETHANE SYSTEMS |
MIL-H-47143 Base Document:1974 | HEAT TREATING, TYPE D6AC ALLOY STEEL, PROCESSED FOR |
MIL-T-8506 Revision A:1966 | TUBING, STEEL, CORROSION-RESISTANT (304) ANNEALED SEAMLESS AND WELDED |
SAE AMS 5363 : 2017 | 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) |
MIL-STD-1877 Revision B:1990 | BRAZING, NICKEL, HIGH TEMPERATURE VACUUM |
MIL-S-24512 Base Document:1975 | STEEL FORGINGS, ALLOY, STRUCTURAL, HIGH YIELD STRENGTH (HY-13O) |
SAE AS 85075 : 2000 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
MIL-R-46509 Revision A:1982 | ROCKET MOTOR, XM30, METAL PARTS FOR |
MIL-B-85107 Revision B:1988 | BEARING, SPIN (SIDEWINDER) |
QQ-S-763 Revision F:1996 | STEEL BARS, WIRE, SHAPES AND FORGINGS; CORROSION RESISTANT |
MIL-E-8697 Revision E:1972 | ELECTRODE, WELDING, COVERED LOW HYDROGEN HEAT TREATABLE STEEL |
MIL-B-81936-1 Revision B:1994 | BEARING, PLAIN, SELF-ALIGNING, BE CU BALL, CRES REACE (WITH STACKING GROOVE) -65 DEG F TO +350 DEG F |
MIL-W-6873 Revision C:1991 | WELDING FLASH CARBON AND ALLOY STEEL |
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 |
MIL-L-40085 Revision F:1989 | LINK ASSEMBLY,TYPE IV, AIR DELIVERY |
NAS159:2002 | BOLT - INTERNAL WRENCHING - AIRCRAFT |
NASA MSFC STD 506 : 1988 | MATERIALS AND PROCESSES CONTROL |
MIL-F-7190 Revision B:1985 | FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
NASA STD 6002 : 2008 | APPLYING DATA MATRIX IDENTIFICATION SYMBOLS ON AEROSPACE PARTS |
MIL K 20277 : H | KNIFE, COMBAT AND SHEATH |
NASM1312-11:2017 | FASTENER TEST METHODS METHOD 11 TENSION FATIGUE |
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 |
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 AS 7101 : 2007 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) GENERAL REQUIREMENTS FOR MATERIALS TEST LABORATORY ACCREDITATION PROGRAM |
SAE AS 23899 : 2012 | AURAL PROTECTOR, SOUND |
API 7K : 2015 | DRILLING AND WELL SERVICING EQUIPMENT |
API 7K REDLINE : 2010 | DRILLING AND WELL SERVICING EQUIPMENT |
SAE AMS 2424 : 2010 | PLATING, NICKEL LOW-STRESSED DEPOSIT |
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 AMS 2759/3 : 2015 | HEAT TREATMENT PRECIPITATION-HARDENING CORROSION-RESISTANT, MARAGING, AND SECONDARY HARDENING STEEL PARTS |
SAE AMS 2418 : 2017 | PLATING, COPPER |
SAE AMS 2759 : 2014 | 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 AMS 2750 : 2012 | PYROMETRY |
MIL-C-14550 Revision B:1983 | COPPER PLATING (ELECTRODEPOSITED) |
ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.