|
SAE AMS 4901 : 2015
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 70.0 KSI (485 MPA) |
|
I.S. EN 4700-007:2010
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
|
ASTM A 1080 : 2015 : REDLINE
|
Standard Practice for Hot Isostatic Pressing of Steel, Stainless Steel, and Related Alloy Castings |
|
BS EN 4700-001:2010
|
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Plate, sheet and strip |
|
SAE AMS 4863 : 2015
|
COPPER-NICKEL-TIN ALLOY CASTINGS, CU - 15NI - 8SN, HOT ISOSTATICALLY PRESSED, SOLUTION ANNEALED AND SPINODAL HEAT TREATED |
|
SAE AMS 4966 : 2017
|
TITANIUM ALLOY, FORGINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
|
MIL-DTL-32477 Base Document:2013
|
Rod and Bar, Cobalt-Nickel-Chromium-Iron-Molybdenum Alloy, for use in Critical Seawater Applications |
|
SAE AMS 2411 : 2013
|
PLATING, SILVER FOR HIGH TEMPERATURE APPLICATIONS |
|
SAE AMS 5934/H1000 : 2015
|
STEEL, EXTRA HIGH TOUGHNESS, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, RINGS, AND EXTRUSIONS 13CR - 8.0NI - 2.2MO - 1.1AL VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, PRECIPITATION HARDENED (H1000) |
|
SAE AMS 6935 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 6.0V - 2.0SN, SOLUTION HEAT TREATED AND AGED |
|
SAE AMS 4916L : 2017
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
|
SAE AS 7237 : 2012
|
RIVETS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT 47.5NI-22CR-1.5CO-9.0MO-0.60W-18.5FE SOLUTION HEAT TREATED PROCUREMENT SPECIFICATION FOR |
|
SAE AMS 5895 : 2015
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1750 DEGREES F (954 DEGREES C) SOLUTION HEAT TREATED, WELDING GRADE, PRECIPITATION HARDENABLE |
|
SAE AMS 2762 : 2018
|
CARBURIZING - CARBON AND LOW-ALLOY STEEL PARTS |
|
SAE AMS 4962 : 2016
|
TITANIUM ALLOY, INVESTMENT CASTINGS, 6 AL - 4 V HOT ISOSTATICALLY PRESSED |
|
SAE AMS 4992 : 2014
|
CASTING, STRUCTURAL INVESTMENT, TITANIUM ALLOY 6AL - 4V HOT ISOSTATICALLY PRESSED |
|
SAE AMS 4511 : 2012
|
COPPER-BERYLLIUM ALLOY CASTINGS 97CU - 2.1BE - 0.52(CO + NI) - 0.28SI SOLUTION AND PRECIPITATION HEAT TREATED (TFOO) |
|
13/30290101 DC : 0
|
BS EN 4700-2 - AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
|
SAE AMS 5843 : 2016
|
COBALT-NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS 19CR - 36CO - 25NI - 7.0MO - 0.50CB (NB) - 2.9TI - 0.20AL - 9.0FE VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, WORK STRENGTHENED, AND AGED |
|
SAE AMS 6327L : 2017
|
STEEL BARS AND FORGINGS, 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740), HEAT TREATED, 125 KSI (862 MPA) TENSILE STRENGTH (COMPOSITION SIMILAR TO UNS G87400) |
|
SAE AMS 4928W : 2017
|
TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
|
SAE AMS 5711 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 65NI - 15.8CR - 15.2MO - 0.30AL - 0.05LA, SOLUTION HEAT TREATED |
|
BS 4S 500:2010
|
Aerospace series. Procedure for inspection, testing and acceptance of steel sheet and strip |
|
BS 3TA 100:2009
|
Procedure for inspection, testing and acceptance of wrought titanium and titanium alloys |
|
SAE AMS 2759/7 : 2010
|
CARBURIZING AND HEAT TREATMENT OF CARBURIZING GRADE STEEL PARTS |
|
SAE AMS 4905 : 2017
|
TITANIUM ALLOY, DAMAGE-TOLERANT GRADE PLATE, 6AL - 4V, BETA ANNEALED |
|
SAE AS 4877 : 2017
|
BOLTS AND SCREWS, NICKEL ALLOY UNS N07718, CLASSIFICATION: 185 KSI/1200 DEGREES F, PROCUREMENT SPECIFICATION |
|
SAE AMS 6932 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V EXTRA LOW INTERSTITIAL, ANNEALED |
|
SAE AMS 6945 : 2014
|
TITANIUM ALLOY, SINGLE MELT, SHEET, STRIP, AND PLATE 6AL - 4V ANNEALED |
|
SAE AMS 6926 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED AND AGED |
|
UNI EN 4700-006 : 2011
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
MIL-DTL-46192 Revision C:1998
|
ALUMINUM ALLOY ARMOR ROLLED PLATE (1/2 TO 4 INCHES THICK), WELDABLE (ALLOY 2519) |
|
MIL-H-6875 Revision H:1989
|
HEAT TREATMENT OF STEEL RAW MATERIALS |
|
SAE AMS 5935 : 2016
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, AND FORGINGS, 12CR - 10NI - 2MO - 0.9AL - 0.3TI, VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
BS 5L 101:2011
|
Procedure for inspection, testing and acceptance of aluminium-base and magnesium-base ingots and castings |
|
BS EN 4700-005:2010
|
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Forging stock |
|
SAE AMS 4990 : 2015
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED AND AGED |
|
SAE AMS 6905 : 2014
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 2.0MO, DUPLEX ANNEALED |
|
SAE AMS 4979J : 2017
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 6947 : 2015
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 4AL - 2.5V -1.5 FE ANNEALED, HEAT TREATABLE |
|
SAE AMS 5663 : 2016
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1775 DEGREES F (968 DEGREES C) SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 6527 : 2018
|
STEEL, BARS AND FORGINGS, 2.0CR - 10NI - 14CO - 1.0MO (0.15 - 0.19C), VACUUM MELTED, NORMALIZED AND OVERAGED |
|
SAE AMS 5223 : 2012
|
IRON-NICKEL ALLOY, STRIP, 49Fe 5.3Cr 42Ni 2.5Ti 0.55Al, SOLUTION HEAT TREATED, COLD ROLLED, 10% REDUCTION |
|
SAE AMS 4970 : 2016
|
TITANIUM ALLOY BARS, WIRE, AND FORGINGS 7AL - 4MO SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 2412 : 2015
|
PLATING, SILVER, COPPER STRIKE, LOW BAKE |
|
SAE AS 7452 : 2014
|
BOLTS AND SCREWS, STEEL, LOW ALLOY HEAT TREATED, ROLL THREADED |
|
SAE MA 3378 : 2018
|
BOLTS AND SCREWS, UNS N07001, TENSILE STRENGTH 1210 MPA, THREAD AND FILLET RADIUS ROLLED BEFORE AGING, PROCUREMENT SPECIFICATION, METRIC |
|
MIL-STD-1881 Base Document:1983
|
BRAZING SILVER, GENERAL PROCESS FOR |
|
UNI EN 4800-006 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
API 2SF : 2013
|
MANUFACTURE OF STRUCTURAL STEEL FORGINGS FOR PRIMARY OFFSHORE APPLICATIONS |
|
SAE AMS 6433 : 2015
|
STEEL, SHEET, STRIP, AND PLATE 0.75MN - 0.78CR - 1.8NI - 0.35MO - 0.20V (0.33 - 0.38C) (4335 MOD) |
|
MIL-DTL-16356 Revision E:2013
|
GAUGES, DIRECT READING, OBLONG GLASS |
|
SAE AS 7235 : 2012
|
RIVETS, UNS S66286, STEEL, CORROSION AND HEAT RESISTANT, 80 KSI SHEAR STRENGTH, PROCUREMENT SPECIFICATION FOR |
|
SAE AMS 4362 : 2014
|
FORGINGS, MAGNESIUM ALLOY, 5.5ZN - 0.45ZR (ZK60A-T5), PRECIPITATION HEAT TREATED |
|
MIL-HDBK-1884 Base Document:1998
|
COATING, PLASMA SPRAY DEPOSITION |
|
MIL-DTL-32505 Revision A:2017
|
ARMOR PLATE, ALUMINUM, ALLOYS 7017 AND 7020, WELDABLE |
|
SAE AMS 5629H : 2016
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, RINGS, AND EXTRUSIONS, 13CR - 8.0NI - 2.2MO - 1.1AL, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 5704 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, FORGINGS 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1825 TO 1900 DEGREES F (996 TO 1038 DEGREES C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
|
SAE AS 7466 : 2014
|
BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, FATIGUE RATED, PROCUREMENT SPECIFICATION |
|
SAE AMS 4965 : 2014
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
|
SAE AMS 5622 : 2013
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE, CONSUMABLE ELECTRODE REMELTED |
|
SAE AMS 4987 : 2015
|
TITANIUM ALLOY, FORGINGS, 10V - 2FE - 3AI, CONSUMABLE ELECTRODE MELTED, SINGLE-STEP SOLUTION HEAT TREATED AND OVERAGED, 140 KSI (965 MPA) TENSILE STRENGTH |
|
PREN 4700-005 : 200P2
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
|
PREN 4800-006 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 6: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
SAE AMS 5655 : 2016
|
STEEL, CORROSION AND HEAT RESISTANT, BARS, WIRE, AND FORGINGS 12.5CR - 0.75NI - 1.0MO - 1.0W - 0.24V (0.20-0.25C) HARDENED AND TEMPERED |
|
SAE AMS 5703 : 2018
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 41.5NI - 16CR - 37FE - 2.9CB - 1.8TI, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1750 DEGREES F (954 DEGREES C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
|
SAE AMS 4304 : 2015
|
ALUMINUM ALLOY, DISCONTINUOUSLY REINFORCED SHEET, 2009/SIC/15W (T8P), SOLUTION HEAT TREATED, STRETCHED, AND PRECIPITATION HEAT TREATED |
|
SAE AMS 4595 : 2011(R2018)
|
COPPER NICKEL TIN ALLOY PLATE, 77CU - 15NI - 8SN, SOLUTION ANNEALED AND SPINODAL HARDENED (TX 00) |
|
PREN 4800-005 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 5: FORGING STOCK |
|
PREN 4700-003 : 200P2
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
|
SAE AMS 4921 : 2016
|
TITANIUM BARS, WIRE, FORGINGS, AND RINGS COMMERCIALLY PURE, 70 KSI (483 MPA) YIELD STRENGTH |
|
PREN 4700-006 : 200P2
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
PREN 4800-003 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 3: TUBE |
|
SAE AS 7228 : 2015
|
RIVETS, STEEL, CORROSION RESISTANT 18CR-9NI, SOLUTION HEAT TREATED, PROCUREMENT SPECIFICATION FOR |
|
SAE AMS 5834 : 2014
|
COBALT ALLOY, CORROSION AND HEAT-RESISTANT, ROUND WIRE 20CR - 15NI - 40CO - 7.0MO - 16FE VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, COLD DRAWN, AND AGED |
|
SAE AMS 5842 : 2016
|
COBALT-NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS 19CR - 36CO - 25NI - 7.0MO - 0.50CB (NB) - 2.9TI - 0.20AL - 9.0FE VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED AND WORK STRENGTHENED |
|
SAE AMS 6915 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 7.0AL - 4.0MO, ANNEALED |
|
SAE AMS 4914 : 2014
|
TITANIUM ALLOY COLD ROLLED SHEET AND STRIP, 15V - 3AL - 3CR - 3SN, SOLUTION HEAT TREATED |
|
SAE AMS 4907 : 2013
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6.0AL - 4.0V, EXTRA LOW INTERSTITIAL, ANNEALED |
|
I.S. EN 4800-002:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
|
SAE MAM 4911 : 1994
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4V, ANNEALED |
|
AWS C3.4M/C3.4 : 2016
|
SPECIFICATION FOR TORCH BRAZING |
|
SAE AMS 4935 : 2017
|
TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, ANNEALED, BETA PROCESSED |
|
SAE AMS 5771 : 2014
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 74NI - 7.0CR - 16.5 MO, SOLUTION HEAT TREATED |
|
SAE AMS 2481K : 2015
|
Phosphate Treatment Antichafing |
|
SAE AMS 5862M:2017
|
STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 15CR - 4.5NI - 0.30CB (NB) - 3.5CU, CONSUMABLE ELECTRODE REMELTED, SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
|
SAE AMS 5734 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C) SOLUTION HEAT TREATED |
|
SAE AMS 6949 : 2016
|
TITANIUM ALLOY, SHEET AND STRIP, 4AL - 2.5V - 1.5FE, ELECTRON BEAM SINGLE MELTED. ANNEALED |
|
SAE AMS 5916 : 2017
|
ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 35FE - 24CR - 37NI - 0.65CB(NB) - 0.2N, ANNEALED |
|
SAE AMS 4994 : 2015
|
TITANIUM ALLOY POWDERED METAL PRODUCTS, 6AL - 4V, HOT ISOSTATICALLY PRESSED, ANNEALED |
|
SAE AMS 6946 : 2014
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE 4AL - 2.5V - 1.5FE, ANNEALED |
|
SAE AMS 5589 : 2013
|
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SEAMLESS TUBING 52.5NI - 19CR - 3.0MO - 5.1CB - 0.90TI - 0.50AL - 18FE CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C), SOLUTION HEAT TREATED |
|
SAE AMS 6920 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
|
SAE AMS 5878 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 59NI - 22CR - 2MO - 14W - 0.35AI - 0.03LA, SOLUTION HEAT TREATED |
|
SAE AS 7102 : 2008
|
NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM, REQUIREMENTS FOR HEAT TREATING |
|
SAE AMS 4903 : 2015
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED |
|
SAE AS 7458 : 2016
|
STUDS, STEEL, LOW ALLOY, HEAT RESISTANT NORMALIZED AND TEMPERED, ROLL THREADED 135000 PSI TENSILE STRENGTH |
|
SAE AMS 4898 : 2014
|
TITANIUM ALLOY, SHEET, 6AL - 2SN - 2ZR - 2MO - 2CR - 0.15SI, ANNEALED |
|
ASTM A 991/A991M : 2017 : REDLINE
|
Standard Test Method for Conducting Temperature Uniformity Surveys of Furnaces Used to Heat Treat Steel Products |
|
NF EN 4700-007 : 2012
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
|
SAE AMS 5643 : 2018
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
MIL-HDBK-1587 Base Document:1996
|
MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
|
MIL-DTL-1222 Revision J:2000
|
STUDS, BOLTS, SCREWS AND NUTS FOR APPLICATIONS WHERE A HIGH DEGREE OF RELIABILITY IS REQUIRED; GENERAL SPECIFICATION FOR |
|
MIL-DTL-25027 Revision H:1997
|
NUT, SELF-LOCKING, 250 DEG F, 450 DEG F, AND 850 DEG F |
|
SAE AS 7229 : 2013
|
RIVETS, STEEL, CORROSION AND HEAT RESISTANT, 18CR - 10.5NI - 0.70(CB+TA), SOLUTION HEAT TREATED, PROCUREMENT SPECIFICATION FOR |
|
SAE AMS 5667 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE EQUALIZED, PRECIPITATION HARDENABLE |
|
SAE AMS 5578 : 2014
|
STEEL, CORROSION AND HEAT-RESISTANT, WELDED TUBING, 12CR - 8.5NI - 0.30CB - 1.1TI - 2.0CU, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE VACUUM MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 2769 : 2014
|
HEAT TREATMENT OF PARTS IN A VACUUM |
|
API SPEC 20E : 2017
|
ALLOY AND CARBON STEEL BOLTING FOR USE IN THE PETROLEUM AND NATURAL GAS INDUSTRIES |
|
BS EN 4700-006:2010
|
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Pre-production and production forgings |
|
SAE AMS 4651 : 2010
|
COPPER-BERYLLIUM, ALLOY, BARS AND RODS - 98CU - 1.9BE, (CDA 172) HARD TEMPER (TD04) |
|
MIL-STD-1876 Revision A:1991
|
NITRIDING, GASEOUS ATMOSPHERE PROCESSING FOR |
|
API 6ACRA : 2015 : ERR 1 : 2015
|
AGE-HARDENED NICKEL-BASED ALLOYS FOR OIL AND GAS DRILLING AND PRODUCTION EQUIPMENT |
|
SAE AMS 5713K : 2016
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 53NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.6AL - 0.006B, VACUUM MELTED, SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 6953 : 2018
|
TITANIUM ALLOY SHEET, 6AL - 4SN - 3NB - 0.5MO - 0.3SI, DUPLEX ANNEALED |
|
SAE AMS 5879 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND FOIL, 62NI - 21.5CR - 9.0MO - 3.7CB (NB), COLD ROLLED AND ANNEALED |
|
SAE AMS 5582 : 2013
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS TUBING, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE TO 155 KSI (1069 MPA) TENSILE STRENGTH |
|
10/30228108 DC : 0
|
BS EN 4400-9 - AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM- AND MAGNESIUM- ALLOYS - TECHNICAL SPECIFICATION - PART 9: PRE-PRODUCTION AND PRODUCTION CASTINGS |
|
SAE AMS H 81200 : 2014
|
HEAT TREATMENT OF TITANIUM AND TITANIUM ALLOYS |
|
BS 5T 100:2010
|
Aerospace series. Procedure for inspection, testing and acceptance of seamless steel tubes and tubestock |
|
MIL-STD-1587 Revision D:2017
|
MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
|
SAE AMS 5442 : 2017
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, NI - 18CR - 2.8MO - 5.5CB(NB) - 0.70TI - 1.50AL - 10FE - 9CO - 1W, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION AND PRECIPITATION HEAT TREATED |
|
EN 4700-002:2016
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002: Bar and section |
|
BS EN 4700-003:2010
|
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Tube |
|
MIL S 1222 : H
|
STUD, BOLTS, HEX CAP SCREWS, SOCKET HEAD CAP SCREWS AND NUTS |
|
SAE AMS 6952 : 2018
|
TITANIUM ALLOY, FORGINGS, 5.8AL - 4.0SN - 3.5ZR - 2.8MO - 0.7NB - 0.35SI - 0.06C, SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 4598 : 2012
|
COPPER NICKEL TIN ALLOY, MECHANICAL TUBE, 77CU - 15NI - 8SN, SOLUTION ANNEALED AND SPINODAL HARDENED (TX 00) |
|
UNI EN 4800-004 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 004: WIRE |
|
NF EN 4700-005 : 2012
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
|
SAE AMS 7482 : 1995
|
STUDS - STEEL, CORROSION AND HEAT RESISTANT,ROLL THREADED AFTER HEAT TREATMENT, 1800F (980 C) SOL HEAT TREATED |
|
UNI EN 4800-005 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
|
I.S. EN 4700-002:2016
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
|
I.S. EN 4700-001:2010
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
|
SAE AMS 5951 : 2017
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 20CR - 10CO - 8.5MO - 2.1TI - 1.5AL - 0.005B, VACUUM INDUCTION AND CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION HEAT TREATABLE |
|
SAE AMS 5709 : 2013
|
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS AND FORGINGS, 58NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1975 DEGREE F (1079 DEGREE C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
|
SAE AMS 5845 : 2014
|
ALLOY, CORROSION-RESISTANT, ROUND BARS 20CR - 35NI - 35CO - 10MO VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE VACUUM REMELTED SOLUTION HEAT TREATED, WORK STRENGTHENED, AND AGED |
|
SAE AMS 4985 : 2014
|
TITANIUM ALLOY, INVESTMENT CASTINGS 6AL - 4V 130 UTS, 120 YS, 6% EL HOT ISOSTATICALLY PRESSED ANNEAL OPTIONAL OR WHEN SPECIFIED |
|
PREN 4700-004 : 200P2
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 4: WIRE |
|
SAE AMS 2417 : 2013
|
PLATING, ZINC-NICKEL ALLOY |
|
SAE AMS 4981 : 2017
|
TITANIUM ALLOY BARS, WIRE, AND FORGINGS, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION AND PRECIPITATION HEAT TREATED |
|
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 AMS 5383 : 2012
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 52.5NI - 19CR - 3.0MO - 5.1CB(NB) - 0.90TI - 0.60AL - 18FE, VACUUM MELTED HOMOGENIZATION AND SOLUTION HEAT TREATED |
|
SAE AMS 4946 : 2016
|
TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC, 3AL - 2.5V, TEXTURE CONTROLLED, COLD WORKED, STRESS RELIEVED |
|
NF EN 4800-003 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE |
|
BS 4HR 100:2010+A1:2012
|
Aerospace series. Procedure for inspection, testing and acceptance of wrought heat-resisting alloys |
|
SAE AMS 5853 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C) SOLUTION TREATED AND WORK-STRENGTHENED, 160 KSI (1103 MPA) TENSILE STRENGTH |
|
SAE AMS 5732 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 5604 J: 2018
|
STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 16.5CR - 4.0NI - 4.0CU - 0.30CB, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 4944 : 2015
|
TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3.0AL - 2.5V COLD WORKED, STRESS RELIEVED |
|
SAE AMS 7725 : 2016
|
TUNGSTEN HEAVY ALLOY SHAPES, SINTERED, HIGH DENSITY |
|
SAE AMS 5841 : 2016
|
COBALT-NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS 19CR - 36CO - 25NI - 7.0MO - 0.50CB (NB) - 2.9TI - 0.20AL - 9.0FE VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED FOR WORK STRENGTHENING |
|
PREN 6070 : 200P1
|
AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS |
|
SAE AMS 6511 : 2012
|
STEEL, MARAGING, BARS, FORGINGS, TUBING, AND RINGS 18NI - 8.5CO - 3.2MO - 0.20TI - 0.10AL DOUBLE VACUUM MELTED, ANNEALED |
|
SAE AMS 2675 : 2013
|
BRAZING, NICKEL ALLOY FILLER METAL |
|
AWS C3.6 : 1999
|
SPECIFICATION FOR FURNACE BRAZING |
|
SAE AMS 5701 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 41.5NI - 16CR - 37FE - 2.9CB (NB) - 1.8TI, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
|
SAE AMS 5536 : 2012
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 47.5NI - 22CR - 1.5CO - 9.0MO - 0.60W - 18.5FE, SOLUTION HEAT TREATED |
|
SAE AS 7236 : 2012
|
RIVETS, ALLOY, CORROSION AND HEAT RESISTANT 52CO-20CR-10NI-15W SOLUTION HEAT TREATED PROCUREMENT SPECIFICATION FOR |
|
NF EN 4800-006 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
SAE AMS 5706 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.006B - 0.05ZR, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1825 TO 1900 DEGREES F SOLUTION HEAT TREATED |
|
NF EN 4800-002 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
|
SAE AMS 2678: 2013
|
FURNACE BRAZING OF PARTS IN A VACUUM ATMOSPHERE |
|
SAE AMS 4911 : 2018
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
|
SAE AMS 2422 : 2014
|
PLATING, GOLD |
|
SAE AMS 5755 : 2014
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 64NI - 5.0CR - 24.5MO - 5.5FE, SOLUTION HEAT TREATED |
|
SAE AMS 5931 : 2012
|
STEEL, BARS, WIRE, FORGINGS, EXTRUSIONS, TUBING, AND RINGS WEAR, GALLING, AND CORROSION RESISTANT - 5.0MN - 3.5SI - 16.5CR - 5.0NI - 0.14N - SOLUTION HEAT TREATED |
|
SAE MA 2538 : 2015
|
GASKET, METAL C-RING SEAL NICKEL ALLOY, CORROSION AND HEAT RESISTANT, METRIC PROCUREMENT SPECIFICATION FOR |
|
SAE AMS 5643/H1100 : 2014
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1100) |
|
SAE AMS 4534 : 2013
|
COPPER-BERYLLIUM ALLOY, BARS AND RODS 98CU - 1.9BE SOLUTION HEAT TREATED, COLD WORKED, AND PRECIPITATION HEAT TREATED (TH04, FORMERLY HT) |
|
SAE AMS 2759 : 2014
|
HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS |
|
SAE AMS 4975 : 2017
|
TITANIUM ALLOY, BARS, WIRE, AND RINGS, 6.0AL - 2.0SN - 4.0ZR - 2.0MO - 0.08SI, SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 5525 : 2012
|
STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED |
|
NF EN 4700-002 : 2012
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
|
SAE AMS 2759/5 : 2004
|
HEAT TREATMENT, MARTENSITIC CORROSION-RESISTANT STEEL PARTS |
|
SAE AMS 5894 : 2016
|
COBALT ALLOYS, BARS, SHEET, AND PLATE, 60CO - 28CR - 4.5W - 1.15C, SOLUTION HEAT TREATED |
|
NAVSEA T9074 BD GIB 010/0300 : 0
|
BASE MATERIALS FOR CRITICAL APPLICATIONS: REQUIREMENTS FOR LOW ALLOY STEEL PLATE, FORGINGS, CASTINGS, SHAPES, BARS, AND HEADS OF HY-80/100/130 AND HSLA-80/100 |
|
MIL-DTL-32528 Base Document:2015
|
Rod, Bar, and Billet, Titanium Alloy TI-5111 for Use in Critical Seawater Application |
|
BS 2B 100:2009
|
Procedure for inspection, testing and acceptance of wrought copper alloys |
|
SAE AMS 6901 : 2015
|
TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
|
SAE AMS 2770 : 2015
|
HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS |
|
BS EN 4700-004:2010
|
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Wire |
|
SAE AMS 6482 : 2015
|
STEEL BARS, FORGINGS, AND TUBING, 1.5SI - 1.25CR - 3.8NI - 0.50MO - 0.30V (0.40C) VACUUM REMELTED, ANNEALED |
|
SAE AMS 4909 : 2016
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
|
SAE AMS 4939C : 2017
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
|
SAE AMS 4259B : 2015
|
ALUMINUM ALLOY, SHEET, 2.4LI - 1.3CU - 0.95MG - 0.10ZR (8090-T6), SOLUTION AND PRECIPITATION HEAT TREATED (UNRECRYSTALLIZED) |
|
SAE AMS 5225 : 2014
|
IRON-NICKEL ALLOY, STRIP, 49FE - 5.3CR - 42NI - 2.5TI - 0.55AL, SOLUTION HEAT TREATED, COLD ROLLED, 50% REDUCTION |
|
NF EN 4800-005 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
|
SAE AMS 4922 : 2014
|
TITANIUM ALLOY, SEAMLESS, HYDRAULIC TUBING 15V - 3.0CR - 3.0AL - 3.0SN COLD WORKED AND PRECIPITATION HEAT TREATED |
|
UNI EN 4700-005 : 2011
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
|
SAE AMS 2772 : 2016
|
HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
|
SAE AS 7108 : 2009
|
NADCAP AUDIT CRITERIA FOR CHEMICAL PROCESSING |
|
BS EN 4700-002:2016
|
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Bar and section |
|
SAE AMS 2759/13 : 2018
|
GASEOUS NITROCARBURIZING |
|
SAE AS 7232 : 2012
|
RIVETS, SOLID AND TUBULAR, NICKEL ALLOY CORROSION AND HEAT RESISTANT 74NI - 15.5CR - 8.0FE PROCUREMENT SPECIFICATION FOR |
|
BS 2HC 100:2010
|
Procedure for inspection, testing and acceptance of iron, nickel, copper, cobalt and refractory metal base alloy castings |
|
UNI EN 4700-004 : 2011
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 004: Wire |
|
BS EN 4800-006:2010
|
Aerospace series. Titanium and titanium alloys. Technical specification Pre-production and production forgings |
|
I.S. EN 4800-005:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
|
SAE AMS 6930 : 2014
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, SOLUTION HEAT TREATED AND AGED |
|
API 16A : 2017
|
SPECIFICATION FOR DRILL-THROUGH EQUIPMENT |
|
BS EN 4800-005:2010
|
Aerospace series. Titanium and titanium alloys. Technical specification Forging stock |
|
API 6DSS : 2017-08
|
SPECIFICATION FOR SUBSEA PIPELINE VALVES |
|
SAE AMS 4919 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 6AL - 2SN - 4ZR - 2MO - 0.08SI DUPLEX ANNEALED |
|
09/30199783 DC : 0
|
BS 4S 500 - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF STEEL SHEET AND STRIP |
|
UNI EN 4800-008 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 008: PRE-PRODUCTION AND PRODUCTION CASTINGS |
|
NF EN 4700-006 : 2012
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
SAE AMS 6951 : 2017
|
TITANIUM ALLOY, SHEET 5AL - 4V - 0.75MO - 0.5FE ANNEALED |
|
SAE AMS 5726 : 2015
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED AND WORK-STRENGTHENED, CONSUMABLE ELECTRODE REMELTED, 200 KSI (1379 MPA) TENSILE STRENGTH CAPABILITY |
|
SAE AMS 5937 : 2012
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, AND FORGINGS, 12CR - 11NI - 2MO - 1.5AL - 0.3TI, VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 4937 : 2014
|
TITANIUM ALLOY, EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 6V - 2SN, BETA EXTRUDED PLUS ANNEALED, HEAT TREATABLE |
|
BS 4HR100(2010):2010
|
AEROSPACE SERIES - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT HEAT-RESISTING ALLOYS |
|
SAE AMS 5938 : 2011
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, AND FORGINGS, 10CR - 12NI - 2MO - 1.45AL - 1.15TI, VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
MIL-M-6857 Revision D:1990
|
MAGNESIUM ALLOY CASTINGS, HEAT TREATMENT OF |
|
SAE AMS 5891 : 2013
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 60NI - 22CR - 2.0MO - 14W - 0.35AL - 0.03LA, ANNEALED |
|
SAE AMS 4871 : 2010(S2015)
|
ALUMINUM BRONZE, CENTRIFUGAL AND CHILL CASTINGS, 85CU - 11AL - 3.6FE, SOLUTION HEAT TREATED AND TEMPERED |
|
SAE AMS 4368 : 2017
|
ALUMINUM ALLOY, DISCONTINUOUSLY REINFORCED HOT ISOSTATICALLY PRESSED SHAPES 6061B/SIC/40P (3[MU]M) (T1P) |
|
SAE AMS 6325 : 2015
|
STEEL, BARS, AND FORGINGS 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) HEAT TREATED, 105 KSI (724 MPA) TENSILE STRENGTH |
|
SAE AMS 2774 : 2016
|
HEAT TREATMENT, WROUGHT NICKEL ALLOY AND COBALT ALLOY PARTS |
|
SAE AS 5270 : 2013
|
BOLTS, SCREWS AND STUDS, NICKEL ALLOY, UNS N07718, WORK-STRENGTHENED, TENSILE STRENGTH 220 KSI, PROCUREMENT SPECIFICATION |
|
SAE AMS 6509A : 2017
|
STEEL BARS AND FORGINGS 3.5CR - 7.5NI - 16.3CO - 1.75MO - 0.2W - (0.09 - 0.13C) DOUBLE VACUUM MELTED, NORMALIZED, ANNEALED |
|
SAE AMS 6520E : 2016
|
STEEL, MARAGING, SHEET, STRIP, AND PLATE, 18NI - 7.8CO - 4.9MO - 0.40TI - 0.10AL, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED |
|
API 6A : 2010
|
SPECIFICATION FOR WELLHEAD AND CHRISTMAS TREE EQUIPMENT |
|
SAE AMS 5934 : 2016
|
STEEL, EXTRA HIGH TOUGHNESS, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, RINGS, AND EXTRUSIONS, 13CR - 8.0NI - 2.2MO - 1.1AL, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
|
SAE AMS 4976 : 2017
|
TITANIUM ALLOY, FORGINGS, 6.0AL - 2.0SN - 4.0ZR - 2.0MO - 08SI, SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 2759/6 : 2005
|
GAS NITRIDING OF LOW-ALLOY STEEL PARTS |
|
SAE AMS 4334 : 2017
|
ALUMINUM ALLOY, FORGINGS 7.8ZN - 2.2MG - 1.6CU - 0.15CR (7249-T74 AND -T7452) |
|
SAE AS 7459 : 2015
|
BOLTS AND SCREWS, STEEL UNS K14675 TENSILE STRENGTH 195 KSI FATIGUE AND STRESS-RUPTURE RATED PROCUREMENT SPECIFICATION |
|
SAE AMS 4417 : 2018
|
CASTINGS, SAND, MAGNESIUM ALLOY, 1.5AG - 2.1DI - 0.08CU - 0.70ZR (EQ21A - T6), SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 5772 E: 2016
|
COBALT ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED |
|
SAE AMS4958E : 2017
|
TITANIUM ALLOY BARS AND RODS, 3AL - 8V - 6CR - 4MO - 4ZR, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED AND CENTERLESS GROUND OR PEELED AND POLISHED |
|
SAE AMS 4917 : 2017
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11CR - 3.0AL - SOLUTION HEAT TREATED |
|
SAE AMS 5854 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, AND RINGS, 61NI - 20.5CR - 8.5MO - 3.4CB(NB) - 1.3TI - 5.0FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED SOLUTION HEAT TREATED |
|
SAE AMS 2685 : 2017
|
WELDING, TUNGSTEN ARC, INERT GAS, (GTAW METHOD) |
|
SAE AS 7455 : 2016
|
BOLTS AND SCREWS, STEEL, LOW ALLOY, HEAT RESISTANT HARDENED AND TEMPERED, ROLL THREADED |
|
SAE AMS 2419 : 2015
|
PLATING, CADMIUM-TITANIUM |
|
SAE AMS 2426E : 2013
|
COATING, CADMIUM VACUUM DEPOSITION |
|
SAE AMS 6517A : 2015
|
STEEL, BARS, AND FORGINGS, 3.5CR - 9.5NI - 18CO - 1.1MO (0.13 - 0.17C) DOUBLE VACUUM MELTED, NORMALIZED, ANNEALED |
|
SAE AMS 5962 : 2012
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, ROUND BARS AND WIRE, 52.5NI - 19CR - 3.0MO - 5.1CB - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION TREATED AND WORK STRENGTHENED, PRECIPITATION HARDENABLE |
|
SAE AMS 4986 : 2015
|
TITANIUM ALLOY, FORGINGS, 10V - 2FE - 3AL, CONSUMABLE ELECTRODE MELTED, SINGLE-STEP SOLUTION HEAT TREATED AND OVERAGED, 160 KSI (1103 MPA) TENSILE STRENGTH |
|
SAE AMS 4596E:2010(R2018)
|
COPPER NICKEL TIN ALLOY, BARS AND RODS, 77CU - 15NI - 8SN, SOLUTION ANNEALED AND SPINODAL HARDENED (TX 00) |
|
SAE AMS 4972 : 2015
|
TITANIUM ALLOY BARS, WIRE, AND RINGS, 8AL - 1MO - 1V, SOLUTION HEAT TREATED AND STABILIZED |
|
SAE AMS 5583 : 2013
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS TUBING 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, VACUUM MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE TO 170 KSI (1172 MPA) TENSILE STRENGTH |
|
SAE AMS 2759/4 : 2008
|
HEAT TREATMENT, AUSTENITIC CORROSION-RESISTANT STEEL PARTS |
|
API 20B : 2013
|
OPEN DIE SHAPED FORGINGS FOR USE IN THE PETROLEUM AND NATURAL GAS INDUSTRY |
|
SAE AMS 5844 : 2014
|
ALLOY, CORROSION-RESISTANT, ROUND BARS, 20CR - 35NI - 35CO - 10MO, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE VACUUM REMELTED, SOLUTION HEAT TREATED AND WORK STRENGTHENED |
|
SAE AS 6414 : 2017
|
MANUFACTURING PROCESSING REQUIREMENTS FOR MOLDED ELASTOMER COMPONENTS USED IN AEROSPACE APPLICATIONS |
|
SAE AS 7471 : 2018
|
BOLTS AND SCREWS, NICKEL ALLOY, UNS N07001 TENSILE STRENGTH 165 KSI, CORROSION AND HEAT RESISTANT, PROCUREMENT SPECIFICATION |
|
SAE AMS 4942 : 2018
|
TITANIUM TUBING, SEAMLESS, ANNEALED, 40.0 KSI (275 MPA) YIELD STRENGTH |
|
SAE AMS 5410 : 2017
|
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 61NI - 16CR - 8.5CO - 1.8MO - 2.6W - 0.85CB (NB) - 3.4TI - 1.8TA - 3.4AL - 0.010B - 0.05ZR, VACUUM MELTED, VACUUM CAST AS CAST, OR SOLUTION TREATED, OR SOLUTION AND PRECIPITATION HARDENED |
|
UNI EN 4700-003 : 2011
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
|
API 16AR : 2017
|
STANDARD FOR REPAIR AND REMANUFACTURE OF DRILL-THROUGH EQUIPMENT |
|
SAE AS 7461 : 2015
|
BOLTS AND SCREWS, TITANIUM ALLOY, 6AL-4V, UNS R56400, FATIGUE-RATED, PROCUREMENT SPECIFICATION FOR |
|
NF EN 4700-003 : 2012
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
|
I.S. EN 4800-004:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 004: WIRE |
|
SAE AMS 5929 : 2014
|
STEEL, CORROSION-RESISTANT, BARS AND FORGINGS, 11.5CR -10NI - 1.0AL - 0.5TI - 1.0CU - 1.0W, VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 4938 : 2013
|
FORGINGS, TITANIUM ALLOYS HEAT-TREATED, FINISHED-PART PROPERTIES: SHORT-TRANSVERSE TENSILE, FRACTURE TOUGHNESS, AND LONGITUDINAL TIME-DEPENDENT-TENSION |
|
API 6D :2015
|
SPECIFICATION FOR PIPELINE AND PIPING VALVES |
|
UNI EN 4800-007 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
|
SAE AMS 4429 : 2012
|
MAGNESIUM ALLOY CASTINGS, SAND 2.8ND - 1.4GD - 0.4ZN - 0.6ZR (EV31A - T6), SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 6532 : 2014
|
STEEL, BARS AND FORGINGS, 3.1CR - 11.5NI - 13.5CO - 1.2MO (0.21 - 0.25C) VACUUM MELTED, NORMALIZED AND OVERAGED, PRECIPITATION HARDENABLE |
|
SAE AMS 6478 : 2001
|
STEEL, BARS AND FORGINGS - 3.1CR - 11.5NI - 13.5CO - 1.2MO (0.21 - 0.25C) VACUUM MELTED, ANNEALED HEAT TREATABLE TO 290 KSI (1999 MPA) TENSILE STRENGTH |
|
SAE AMS 5643/H1025 : 2014
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1025) |
|
SAE AMS 5659/H1025 : 2013
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, RINGS, AND EXTRUSIONS, 15CR - 4.5NI - 0.30CB (NB) - 3.5CU, CONSUMABLE REMELTED, SOLUTION AND PRECIPITATION HEAT TREATED (H1025) |
|
SAE AMS 5643/H1150 : 2013
|
STEEL, CORROSION RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1150) |
|
UNI EN 4700-007 : 2011
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
|
I.S. EN 4700-006:2010
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
NASA HDBK 6025 : 2014
|
GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS |
|
SAE AMS 5441 : 2016
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, NI - 18CR - 2.8MO - 5.5CB(NB) - 0.70TI - 1.50AL - 10FE - 9CO - 1W, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
|
SAE AMS 4973 : 2016
|
TITANIUM ALLOY FORGINGS, 8AL - 1MO - 1V, SOLUTION HEAT TREATED AND STABILIZED |
|
UNI EN 4800-001 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
|
SAE AMS 6439 : 2016
|
STEEL SHEET, STRIP, AND PLATE, 1.05CR - 0.55NI - 1.0MO - 0.12V (0.42 - 0.48C) (D6AC), CONSUMABLE ELECTRODE VACUUM MELTED, ANNEALED |
|
API 2SC : 2010
|
MANUFACTURE OF STRUCTURAL STEEL CASTINGS FOR PRIMARY OFFSHORE APPLICATIONS |
|
SAE AMS 5731 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
|
SAE AMS 5668 : 2012
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 72NI - 15.5CR - 7.0FE - 2.5TI - 1.0CB (NB) - 0.70AL, 2100 DEGREES F (1149 DEGREES C) SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS QQ P 416 : 2016
|
PLATING, CADMIUM (ELECTRODEPOSITED) |
|
API 6D RUSSIAN : 2014
|
SPECIFICATION FOR PIPELINE VALVES |
|
SAE AMS 4232 : 2012
|
ALUMINUM ALLOY EXTRUSIONS, 2.7CU - 2.2LI - 0.12ZR (2090-T86), SOLUTION HEAT TREATED, COLD WORKED, AND PRECIPITATION HEAT TREATED |
|
NF EN 4800-008 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 008: PRE-PRODUCTION AND PRODUCTION CASTINGS |
|
NF EN 4800-007 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
|
BS EN 4800-008:2010
|
Aerospace series. Titanium and titanium alloys. Technical specification Pre-production and production castings |
|
SAE AMS 5744 : 2013
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 15.5CR - 4.5NI - 2.9MO - 0.10N, HEAT TREATED, 170 KSI (1172 MPA) TENSILE STRENGTH |
|
API SPEC 19OH : 2018
|
OPENHOLE ISOLATION EQUIPMENT |
|
SAE AMS 2759/1 : 2009
|
HEAT TREATMENT OF CARBON AND LOW-ALLOY STEEL PARTS, MINIMUM TENSILE STRENGTH BELOW 220 KSI (1517 MPA) |
|
API STD 20J : 2017
|
QUALIFICATION OF DISTRIBUTORS OF METALLIC MATERIALS FOR USE IN THE PETROLEUM AND NATURAL GAS INDUSTRIES |
|
SAE AMS 4940 : 2017
|
TITANIUM SHEET, STRIP, AND PLATE COMMERCIALLY PURE ANNEALED, 25.0 KSI (172 MPA) YIELD STRENGTH |
|
MIL-STD-1884 Revision A:1991
|
COATING, PLASMA SPRAY DEPOSITION |
|
SAE AMS 2773 : 2013
|
HEAT TREATMENT, CAST NICKEL ALLOY AND COBALT ALLOY PARTS |
|
UNI EN 4800-003 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE |
|
SAE AMS 5737 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 6512 H : 2017
|
STEEL, MARAGING, BARS, FORGINGS, TUBING, AND RINGS 18NI - 7.8CO - 4.9MO - 0.40TI - 0.10AL CONSUMABLE ELECTRODE VACUUM MELTED, ANNEALED |
|
SAE AMS 5629/H1000 : 2015
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, RINGS, AND EXTRUSIONS, 13CR - 8.0NI - 2.2MO - 1.1AL, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENED (H1000) |
|
SAE AMS 5915 : 2014
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 57NI - 20CR - 10CO - 8.5MO - 2.1TI - 1.5AL - 0.005B, VACUUM INDUCTION AND CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION HEAT TREATABLE |
|
SAE AMS 2413 : 2013
|
PLATING, SILVER-RHODIUM |
|
SAE AMS 5671 : 2013
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 5940 : 2014
|
ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 34CO - 3.0CR - 28NI - 3.0CB(NB) - 5.5AL - 0.008B - 25.5FE MULTIPLE MELTED, HIGH TEMPERATURE, OXIDATION-RESISTANT, LOW EXPANSION SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
|
MIL-DTL-46118 Revision E:1998
|
ALUMINUM ALLOY ARMOR, 2219, ROLLED PLATE AND DIE FORGED SHAPES |
|
SAE AMS 4926 : 2015
|
TITANIUM ALLOY, BARS, WIRE, AND RINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
|
SAE AMS5659S : 2016
|
Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu
|
|
SAE AMS 6936 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6AL - 6V - 2SN, ANNEALED |
|
SAE AS 7456 : 2016
|
STUDS, STEEL, LOW ALLOY, HEAT TREATED, ROLL THREADED |
|
SAE AMS 2757 : 2010
|
GASEOUS NITROCARBURIZING |
|
BS EN 4800-001:2010
|
Aerospace series. Titanium and titanium alloys. Technical specification Plate, sheet and strip |
|
BS 5L100(2011) : 2011
|
PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT ALUMINIUM AND ALUMINIUM ALLOYS |
|
AWS C3.7 : 1999
|
SPECIFICATION FOR ALUMINUM BRAZING |
|
SAE AMS 5810 : 2015
|
STEEL, CORROSION AND HEAT RESISTANT, FLAT WIRE, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREES F (982 DEGREES C) SOLUTION TREATED, COLD DRAWN OR COLD ROLLED AND AGED, CONSUMABLE ELECTRODE REMELTED |
|
BS EN 4800-004:2010
|
Aerospace series. Titanium and titanium alloys. Technical specification Wire |
|
API 14A : 2015
|
SPECIFICATION FOR SUBSURFACE SAFETY VALVE EQUIPMENT |
|
11/30253929 DC : 0
|
BS EN 4820 - AEROSPACE SERIES - COPPER AND COPPER ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION |
|
BS EN 4800-002:2010
|
Aerospace series. Titanium and titanium alloys. Technical specification Bar and section |
|
BS EN 4800-003:2010
|
Aerospace series. Titanium and titanium alloys. Technical specification Tube |
|
SAE AMS 5708 : 2015
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, WIRE FORGINGS, AND RINGS, 58NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1975 DEGREES F (1079 DEGREES C) SOLUTION HEAT TREATED |
|
MIL-H-6088 Revision G:1991
|
HEAT TREATMENT OF ALUMINIUM ALLOYS |
|
SAE AMS 5746 : 2012
|
ALLOY, CORROSION AND HEAT RESISTANT, BARS AND FORGINGS - 15CR - 45NI - 4.1MO - 4.1W - 3.0TI - 1.0AL - 31FE (D979) CONSUMABLE ELECTRODE VACUUM MELTED, SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 5622/H1025 : 2015
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS 16CR - 4.0NI - 0.30CB - 4.0CU SOLUTION HEAT TREATED, PRECIPITATION HARDENED (H1025) CONSUMABLE ELECTRODE REMELTED |
|
NF EN 4700-001 : 2012
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
|
API 20A : 2017
|
CARBON STEEL, ALLOY STEEL, STAINLESS STEEL, AND NICKEL BASE ALLOY CASTINGS FOR USE IN THE PETROLEUM AND NATURAL GAS INDUSTRY |
|
SAE AMS 4920 : 2015
|
TITANIUM ALLOY, FORGINGS, 6AI - 4V, ALPHA-BETA OR BETA PROCESSED, ANNEALED |
|
NF EN 4700-004 : 2012
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 004: WIRE |
|
SAE AS 7109/5 : 2017
|
NAPCAP REQUIREMENTS FOR COATING EVALUATION LABORATORY PRACTICES |
|
SAE AMS 2771 : 2017
|
HEAT TREATMENT OF ALUMINUM ALLOY CASTINGS |
|
SAE AMS 5884 : 2016
|
IRON-NICKEL ALLOY, BARS, FORGINGS, AND RINGS, 42FE - 37.5NI - 14CO - 4.8CB(NB) - 1.6TI, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE MULTIPLE MELTED, HIGH TEMPERATURE, LOW EXPANSION |
|
SAE AMS 4303 : 2017
|
ALUMINUM ALLOY PLATE, 2.7CU - 2.2LI - 0.12ZR (2090-T81), SOLUTION HEAT TREATED, COLD WORKED, AND AGED |
|
SAE AMS5337E : 2017
|
STEEL, MARAGING, INVESTMENT CASTINGS, 18.5NI - 9.0CO - 5.0MO - 0.70TI - 0.12AL, VACUUM MELTED, HOMOGENIZED, OVERAGED, AND SOLUTION HEAT TREATED |
|
SAE AMS 5368 : 2012
|
STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS 15CR - 4.0NI - 2.3MO - 0.09N SOLUTION HEAT TREATED |
|
SAE AMS 4915 : 2017
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1V - 1MO SINGLE ANNEALED |
|
SAE AMS4897D : 2016
|
TITANIUM ALLOY, SHEET AND STRIP, 15MO - 3.0AL - 2.8CB - 0.20SI |
|
SAE AMS 5399 : 2012
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 52NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.6AL - 0.006B, VACUUM-MELTED, VACUUM-CAST, SOLUTION HEAT TREATED |
|
SAE AMS 5608 : 2016
|
COBALT ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED |
|
NF EN 4800-004 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 004: WIRE |
|
SAE AMS 4893 : 2017
|
ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, SOLUTION TREATED |
|
SAE AMS 6925 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 13V - 11CR - 3AL, SOLUTION HEAT TREATED |
|
SAE AMS 4989 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 3AL - 2.5V, ANNEALED |
|
SAE AMS 5759M : 2015
|
COBALT ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGING STOCK, FORGINGS, AND RINGS 52CO - 20CR - 10NI - 15W |
|
SAE AS 7475 : 2015
|
BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30159, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
|
SAE AMS4933F : 2017
|
TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS 8AL - 1MO - 1V SOLUTION HEAT TREATED AND STABILIZED |
|
SAE AMS 6948 : 2015
|
TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 4AL - 2.5V -1.5 FE, ANNEALED |
|
SAE AMS 6519 : 2014
|
STEEL, MARAGING, BARS, FORGINGS, TUBING, AND RINGS 19NI - 3.0MO - 1.4TI - 0.10AL PREMIUM AIRCRAFT QUALITY DOUBLE VACUUM MELTED, ANNEALED |
|
SAE AMS 6525 : 2016
|
STEEL, BARS, FORGINGS, TUBING, AND RINGS, 0.75CR - 9.0NI - 4.5CO - 1.0MO - 0.09V (0.17 - 0.23C), CONSUMABLE ELECTRODE VACUUM MELTED |
|
SAE AMS 6516 : 2017
|
STEEL, BARS AND FORGINGS 1CR - 10NI - 7CO - 2MO - 1.3W - 0.1V - (0.28 - 0.32C) VACUUM INDUCTION MELTED, VACUUM ARC REMELTED, NORMALIZED AND ANNEALED PRECIPITATION HARDENABLE |
|
SAE AS 7109/3 : 2017
|
NADCAP REQUIREMENTS FOR DIFFUSION COATING PROCESSES |
|
SAE AMS 4918 : 2014
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, ANNEALED |
|
SAE AMS 4904 : 2015
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
|
SAE AMS 5662 : 2016
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AI - 18FE CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
|
SAE AMS 4881 : D2012(R2018)
|
NICKEL-ALUMINUM-BRONZE, MARTENSITIC, SAND, CENTRIFUGAL AND CONTINUOUS CASTINGS, 78CU - 11AL - 5.1NI - 4.8FE, QUENCH HARDENED AND TEMPER ANNEALED |
|
PREN 4800-008 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 8: PRE-PRODUCTION AND PRODUCTION CASTINGS |
|
SAE AMS 4535 : 2015
|
COPPER-BERYLLIUM ALLOY, MECHANICAL TUBING 98CU - 1.9BE SOLUTION AND PRECIPITATION HEAT TREATED (TF00, FORMERLY AT) |
|
PREN 4800-002 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 2: BAR AND SECTION |
|
SAE AMS 4442 : 2012
|
MAGNESIUM ALLOY SAND CASTINGS, 3.2 RARE EARTHS - 2.5ZN - 0.70ZR (EZ33A-T5), PRECIPITATION HEAT TREATED |
|
API 20H : 2015
|
HEAT TREATMENT SERVICES - BATCH TYPE FOR EQUIPMENT USED IN THE PETROLEUM AND NATURAL GAS INDUSTRY |
|
SAE AMS 5917 : 2011
|
METAL INJECTION MOLDED NICKEL BASED, ALLOY 718 PARTS, HOT ISOSTATICALLY PRESSED, SOLUTIONED AND AGED |
|
SAE AMS 5707 : 2017
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED 1825 TO 1900 DEGREES F (996 TO 1038 DEGREES C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
|
SAE AS 7472 : 2015
|
BOLTS AND SCREWS, STEEL, CORROSION RESISTANT 125000 PSI TENSILE STRENGTH ROLL THREADED |
|
SAE AMS 4371 : 2015
|
MAGNESIUM ALLOY, PLATE, 4.0Y - 2.25ND - 0.5ZR (WE43C - T5), PRECIPITATION HEAT TREATED |
|
SAE AMS 5833 : 2014
|
COBALT ALLOY, CORROSION AND HEAT-RESISTANT, ROUND WIRE 20CR - 15NI - 40CO - 7.0MO - 16FE SOLUTION HEAT TREATED AND COLD DRAWN |
|
SAE AMS 6543 : 2016
|
STEEL, BARS AND FORGINGS, 2.0CR - 10NI - 8.0CO - 1.0MO (0.10 - 0.14C) (HY-180), DOUBLE VACUUM MELTED, SOLUTION HEAT TREATED, MARAGE HARDENABLE |
|
AWS C3.9M/C3.9 : 2009
|
SPECIFICATION FOR RESISTANCE BRAZING |
|
SAE AS 7467 : 2013
|
BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, STRESS RUPTURE RATED, PROCUREMENT SPECIFICATION |
|
SAE AMS 5768 : 2018
|
ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 21CR - 20NI - 20CO - 3.0MO - 2.5W - 1.0CB - 0.15N - 31FE, SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 4485A : 2017
|
MAGNESIUM ALLOY, EXTRUSIONS 4.0Y - 2.25ND - 0.5ZR (WE43C - T5) PRECIPITATION HEAT TREATED |
|
SAE AMS QQ N 290 : 2015
|
NICKEL PLATING (ELECTRODEPOSITED) |
|
SAE AS 7454 : 2016
|
BOLTS AND SCREWS, STEEL, LOW ALLOY, HEAT RESISTANT 135000 PSI TENSILE STRENGTH, NORMALIZED AND TEMPERED, ROLL THREADED |
|
NF EN 4800-001 : 2012
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
|
SAE AMS 5876 : 2018
|
COBALT ALLOY, CORROSION AND HEAT-RESISTANT, STRIP, 20CR - 15NI - 40CO - 7.0MO - 16FE, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE REMELTED, SOLUTION HEAT TREATED AND COLD ROLLED |
|
SAE AMS 5763E : 2016
|
STEEL, CORROSION RESISTANT BARS, FORGINGS, TUBING, AND RINGS, 15CR - 6.5NI - 0.75MO - 0.50CB (NB) - 1.5CU, SOLUTION HEAT TREATED |
|
SAE AMS 2801 : 2014
|
HEAT TREATMENT OF TITANIUM ALLOY PARTS |
|
SAE AMS 2428 : 2017
|
PLATING, COBALT-PHOSPHORUS, NANOCRYSTALLINE |
|
SAE AMS 4941 G : 2017
|
TITANIUM TUBING, WELDED, 40 KSI (276 MPA) YIELD STRENGTH |
|
SAE AMS 5919 : 2013
|
COBALT-NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, ROUND BARS 19CR - 36CO - 25NI - 7.0MO - 0.50CB (NB) - 2.9TI - 0.20AL - 9.0FE VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED AND WORK STRENGTHENED, MODIFIED STRENGTH |
|
SAE AMS 4910 : 2017
|
TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN ANNEALED |
|
SAE AMS 5955 : 2016
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, AND FORGINGS 10CR - 12NI - 2MO - 1.45AL - 1.15TI VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
NASA MSFC SPEC 3717 : 2017
|
SPECIFICATION FOR CONTROL AND QUALIFICATION OF LASER POWDER BED FUSION METALLURGICAL PROCESSES |
|
SAE AMS 5670 : 2012
|
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS - 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 4999 : 2016
|
TITANIUM ALLOY DIRECT DEPOSITED PRODUCTS, 6AL - 4V, ANNEALED |
|
UNI EN 4700-001 : 2011
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
|
I.S. EN 4700-005:2010
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 005: FORGING STOCK |
|
EN 4800-003:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 003: Tube |
|
EN 4800-002:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section |
|
EN 4800-001:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 001: Plate, sheet and strip |
|
EN 4700-005:2010
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 005: Forging stock |
|
EN 4700-003:2010
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 003: Tube |
|
EN 4700-007:2010
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 007: Remelting stock |
|
EN 4800-004:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 004: Wire |
|
EN 4800-006:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 006: Pre-production and production forgings |
|
EN 4800-008:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 008: Pre-production and production castings |
|
EN 4800-007:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 007: Remelting stock |
|
EN 4800-005:2010
|
Aerospace series - Titanium and titanium alloys - Technical specification - Part 005: Forging stock |
|
EN 4700-004:2010
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 004: Wire |
|
EN 4700-001:2010
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 001: Plate, sheet and strip |
|
EN 4700-006:2010
|
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 006: Pre-production and production forgings |
|
SAE AS 7460 : 2017
|
BOLTS AND SCREWS, TITANIUM ALLOY, 6.0AL-4.0V, PROCUREMENT SPECIFICATION FOR |
|
MIL-DTL-32375 Revision B:2017
|
Armor Plate, Aluminum Alloy, 7085, 7056, 7075, 7181, and 7099, Unweldable Applique |
|
AWS C3.6M/C3.6 : 2016
|
SPECIFICATION FOR FURNACE BRAZING |
|
SAE AMS 7735 : 2018
|
ALLOY WIRE, ROUND, 35PD - 30AG - 14CU - 10AU - 10PT - 0.85ZN, SOLUTION HEAT TREATED |
|
SAE AMS 6910 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 8AL - 1MO - 1V, DUPLEX ANNEALED |
|
SAE AMS 4250 : 2018
|
ALUMINUM ALLOY, PLATE - 8.1ZN - 2.3MG - 1.0CU - ZR (7449-T7651) SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
|
SAE AMS 6526 : 2016
|
STEEL, BARS, FORGINGS, TUBING, AND RINGS, 1.0CR - 7.5NI - 4.5CO - 1.0MO - 0.09V (0.29 - 0.34C), CONSUMABLE ELECTRODE VACUUM REMELTED, ANNEALED |
|
SAE AS 7468 : 2012
|
BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30035, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
|
SAE AMS 4355 : 2015
|
ALUMINUM ALLOY, DISCONTINUOUSLY REINFORCED HOT ISOSTATICALLY PRESSED SHAPES 2124A/SIC/25P (3[MU]M) (T1P) |
|
SAE AMS 4880 : 2011
|
ALUMINUM BRONZE ALLOY, CENTRIFUGAL AND CONTINUOUS-CAST CASTINGS - 81.5CU - 10.3AL - 5.0NI - 2.8FE QUENCH HARDENED AND TEMPER ANNEALED (TQ50) |
|
SAE MAM 5706 : 2003
|
ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT, 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4A1 - 0.006B - 0.05ZR, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 995 DEGREES - 1040 DEGREES C SOLUTION HEAT TREATED |
|
API 6ACRA : 2015 : INC : ADD 1 : 2017
|
AGE-HARDENED NICKEL-BASED ALLOYS FOR OIL AND GAS DRILLING AND PRODUCTION EQUIPMENT |
|
SAE AMS 6900 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 5AL - 2.5SN, ANNEALED |
|
SAE ARP 5144 : 2017
|
HEAT APPLICATION FOR THERMOSETTING RESIN CURING |
|
SAE MAM 4427 : 2003
|
MAGNESIUM ALLOY SAND CASTINGS 4.0Y - 2.3ND - 0.7ZR (WE43A - T6) SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 4943 : 2015
|
TITANIUM ALLOY, HYDRAULIC, SEAMLESS TUBING, 3.0AL - 2.5V, ANNEALED |
|
SAE AMS 6522 : 2016
|
STEEL PLATE 2.0CR - 10NI - 14CO - 1.0MO (0.13 - 0.17C) VACUUM MELTED, NORMALIZED, AND OVERAGED |
|
SAE AMS 4352J : 2017
|
MAGNESIUM ALLOY, EXTRUSIONS, 5.5ZN - 0.45ZR (ZK60A - T5), PRECIPITATION HEAT TREATED |
|
SAE AMS 2768 : 2010
|
HEAT TREATMENT OF MAGNESIUM ALLOY CASTINGS |
|
I.S. EN 4700-003:2010
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 003: TUBE |
|
I.S. EN 4800-006:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 006: PRE-PRODUCTION AND PRODUCTION FORGINGS |
|
SAE AMS 5922 : 2015
|
STEEL, CORROSION-RESISTANT, BARS, AND FORGINGS, 10CR - 5.5NI - 14CO - 2MO - 1W (0.19-0.23C), VACUUM INDUCTION MELTED, VACUUM ARC REMELTED, NORMALIZED, ANNEALED |
|
SAE AMS 4426 : 2013
|
CASTINGS, SAND, MAGNESIUM ALLOY 5.1Y - 3.0RE - 0.70ZR (WE54-T6) SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 4931 : 2015
|
TITANIUM ALLOY BARS, FORGINGS, AND RINGS, 6AL - 4V EXTRA LOW INTERSTITIAL (ELI), DUPLEX ANNEALED, FRACTURE TOUGHNESS |
|
SAE AMS 4988 : 2014
|
TITANIUM ALLOY SHEET, STRIP, AND PLATE, 6AL - 6V - 2SN, SOLUTION HEAT TREATED |
|
BS 6S 100:2010
|
Aerospace series. Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
|
BS EN 4700-007:2010
|
Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Remelting stock |
|
SAE AMS 4967 : 2014
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
|
SAE AMS 5360 : 2012
|
STEEL, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 17CR - 13NI - 1.9MO, SOLUTION HEAT TREATED |
|
I.S. EN 4800-003:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE |
|
09/30201792 DC : 0
|
BS 2HC 100 - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF IRON, NICKEL, COPPER, COBALT AND REFRACTORY METAL BASE ALLOY CASTINGS |
|
SAE AMS 4983 : 2015
|
TITANIUM ALLOY, FORGINGS, 10V - 2FE - 3AL, CONSUMABLE ELECTRODE MELTED, SINGLE-STEP SOLUTION HEAT TREATED AND AGED, 180 KSI (1241 MPA) TENSILE STRENGTH |
|
SAE AMS 4427 : 2012
|
MAGNESIUM ALLOY CASTINGS, SAND, 4.0Y - 2.3ND - 0.7ZR (WE43B - T6), SOLUTION AND PRECIPITATION HEAT TREATED |
|
SAE AMS 7498 : 2016
|
RINGS, FLASH WELDED TITANIUM AND TITANIUM ALLOYS |
|
09/30199785 DC : 0
|
BS 6S 100 - PROCEDURE FOR INSPECTION, TESTING AND ACCEPTANCE OF WROUGHT STEELS (OTHER THAN PLATE, SHEET, STRIP AND TUBE) |
|
SAE AMS 4978 : 2018
|
TITANIUM ALLOY BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED |
|
SAE AMS 5660 : 2015
|
NICKEL-IRON ALLOY, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 12.5CR - 42.5NI - 6.0MO - 2.7TI - 0.015B - 34FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
|
SAE AMS 5858 : 2015
|
STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, MULTIPLE MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED, WELDING GRADE, PRECIPITATION HARDENABLE |
|
SAE AMS 4971L : 2017
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED, HEAT TREATABLE |
|
BS EN 4800-007:2010
|
Aerospace series. Titanium and titanium alloys Remelting stock |
|
SAE AMS 6950 : 2017
|
TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK 4AL - 2.5V - 1.5 FE SINGLE HEARTH MELTED, ANNEALED |
|
SAE AMS 6515 : 2012
|
STEEL, MARAGING, BARS, FORGINGS, TUBING, AND RINGS 18.5NI - 12.0CO - 4.9MO - 1.40TI - 0.10AL DOUBLE VACUUM MELTED, ANNEALED |
|
MIL-DTL-32341 Revision A:2015
|
ARMOR PLATE, ALUMINUM, ALLOY 2139 WELDABLE & ALLOY 2195 AND 2060 UNWELDABLE APPLIQUE |
|
I.S. EN 4800-007:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
|
SAE AMS 5758 : 2014
|
ALLOY, CORROSION-RESISTANT, BARS, 20CR - 35NI - 35CO - 10MO, VACUUM INDUCTION PLUS CONSUMABLE ELECTRODE VACUUM REMELTED, SOLUTION HEAT TREATED FOR WORK STRENGTHENING |
|
SAE AMS 4963 : 2016
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL - 4.0V, ANNEALED, HEAT TREATABLE, MODIFIED STRENGTH |
|
SAE AS 7470 : 2012
|
BOLTS AND SCREWS, STEEL, CORROSION AND MODERATE HEAT RESISTANT HEAT TREATED, ROLL THREADED |
|
AWS C3.7M/C3.7 : 2011
|
SPECIFICATION FOR ALUMINUM BRAZING |
|
MIL-STD-3021 Base Document:2008
|
MANUFACTURING PROCESS STANDARD - MATERIALS DEPOSITION, COLD SPRAY |
|
PREN 4800-001 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 1: PLATE, SHEET AND STRIP |
|
SAE AMS 6907 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, DUPLEX ANNEALED |
|
SAE AMS 2423 : 2015
|
PLATING, NICKEL, HARD DEPOSIT |
|
API STD 6ACRA:2015
|
AGE-HARDENED NICKEL-BASED ALLOYS FOR OIL AND GAS DRILLING AND PRODUCTION EQUIPMENT |
|
MIL-STD-40002 Base Document:1991
|
HEAT TREATMENT CODING SYSTEM, GENERAL |
|
SAE AMS 5712 : 2016
|
NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 53NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.6AL - 0.006B, VACUUM MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 4991 : 2014
|
TITANIUM ALLOY CASTINGS, INVESTMENT 6AL - 4V HOT ISOSTATIC PRESSED, ANNEAL OPTIONAL |
|
SAE AMS 5773 : 2012
|
STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 15CR - 6.5NI - 0.75MO - 0.30 CB (NB) - 1.5CU, CONSUMABLE ELECTRODE REMELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
SAE AMS 6317K : 2017
|
STEEL BARS AND FORGINGS, 1.8NI - 0.25MO (0.38 - 0.43C) (4640), HEAT TREATED, 125 KSI (862 MPA) TENSILE STRENGTH |
|
SAE AMS 6514 : 2017
|
STEEL, MARAGING, BARS, FORGINGS, TUBING, AND RINGS 18.5NI - 9.0CO - 4.9MO - 0.65TI - 0.10AL CONSUMABLE ELECTRODE VACUUM MELTED, ANNEALED |
|
PREN 4800-007 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 7: REMELTING STOCK |
|
SAE AMS 4533 : 2013
|
COPPER-BERYLLIUM ALLOY, BARS AND RODS, 98CU - 1.9BE, SOLUTION AND PRECIPITATION HEAT TREATED (TF00, FORMERLY AT) |
|
SAE AMS 4924 : 2015
|
TITANIUM ALLOY BARS, FORGINGS, AND RINGS-15, 5AL - 2.5SN, EXTRA LOW INTERSTITIAL, ANNEALED |
|
SAE AMS 2759/2 : 2010
|
HEAT TREATMENT OF LOW-ALLOY STEEL PARTS MINIMUM TENSILE STRENGTH 220 KSI (1517 MPA) AND HIGHER |
|
SAE AMS 4957 : 2016
|
TITANIUM ALLOY, ROUND BAR AND WIRE, 3AI - 8V - 6CR - 4MO - 4ZR, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED AND COLD DRAWN |
|
SAE AMS 5877 : 2012
|
IRON ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 29FE - 22CR - 21NI - 18.5CO - 3.2MO - 2.8W - 0.78TA - 0.30AL - 0.05LA - 0.20N, SOLUTION HEAT TREATED |
|
SAE AS 7101 : 2007
|
NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) GENERAL REQUIREMENTS FOR MATERIALS TEST LABORATORY ACCREDITATION PROGRAM |
|
SAE AMS H 6088 : 2000
|
HEAT TREATMENT OF ALUMINUM ALLOYS |
|
SAE AMS 4900 : 2014
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 55.0 KSI (379 MPA) YIELD STRENGTH |
|
PREN 4700-007 : 200P2
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 007: REMELTING STOCK |
|
SAE AMS 5859 : 2012
|
STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 15CR - 6.5NI - 0.75MO - 0.30CB - 1.5CU, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
|
API SPEC 19AC : 2016
|
SPECIFICATION FOR COMPLETION ACCESSORIES |
|
SAE AMS 4902 : 2013
|
TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY-PURE, ANNEALED 40.0 KSI (276 MPA) YIELD STRENGTH |
|
SAE AMS 2728 : 2012
|
HEAT TREATMENT OF WROUGHT COPPER BERYLLIUM ALLOY PARTS |
|
SAE AMS 5661 : 2012
|
NICKEL-IRON ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS - 42.5NI - 12.5CR - 5.8MO - 2.9TI - 0.015B - 35FE - CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
|
PREN 4800-004 : 200P2
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 4: WIRE |
|
PREN 4700-001 : 200P2
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
|
SAE AMS 4930 : 2015
|
TITANIUM ALLOY BARS, WIRE, FORGINGS, AND RINGS, 6AL - 4V, EXTRA LOW INTERSTITIAL, ANNEALED |
|
SAE AS 7112/6 : 2013
|
NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM, TITANIUM 3AL-2.5V ALLOY, SEAMLESS HYDRAULIC TUBING, MANUFACTURING REQUIREMENTS |
|
SAE AMS 6523H : 2017
|
STEEL, SHEET, STRIP, AND PLATE, 0.75CR - 9.0NI - 4.5CO - 1.0MO - 0.09V (0.17 - 0.23C) VACUUM CONSUMABLE ELECTRODE MELTED, ANNEALED |
|
PREN 4700-002 : 200P3
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
|
API 16A : 2017 : INC : ERR 1+ERR2+ADD1 : 2018
|
SPECIFICATION FOR DRILL-THROUGH EQUIPMENT |
|
UNI EN 4800-002 : 2011
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 002: BAR AND SECTION |
|
SAE AMS 4950 : 2015
|
TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL - 4.0V, SOLUTION HEAT TREATED AND AGED, MODIFIED STRENGTH |
|
AWS C3.5M/C3.5 : 2016
|
SPECIFICATION FOR INDUCTION BRAZING |
|
SAE AMS 2767 : 2013
|
UPHILL QUENCHING OF ALUMINUM ALLOY PRODUCT |
|
SAE AMS 6257 : 2016
|
STEEL BARS, FORGINGS, AND TUBING, 1.6SI - 0.82CR - 1.8NI - 0.40MO - 0.08V (0.40 - 0.44C), CONSUMABLE ELECTRODE VACUUM REMELTED, NORMALIZED AND TEMPERED |
|
SAE AMS 4650 : 2013
|
COPPER-BERYLLIUM ALLOY, BARS, RODS, SHAPES, AND FORGINGS 98CU - 1.9BE SOLUTION HEAT TREATED TB00 (A) |
|
SAE AMS 2376 : 2017
|
QUALIFICATION, APPROVAL, AND CONTROL OF PREMIUM-QUALITY FORGINGS ALLOY STEELS AND HEAT-TREATABLE CORROSION AND HEAT RESISTANT STEELS AND ALLOYS |
|
SAE AMS 6921 : 2015
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED AND AGED |
|
SAE AMS 4945 : 2014
|
TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED |
|
I.S. EN 4800-001:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 001: PLATE, SHEET AND STRIP |
|
I.S. EN 4800-008:2010
|
AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 008: PRE-PRODUCTION AND PRODUCTION CASTINGS |
|
I.S. EN 4700-004:2010
|
AEROSPACE SERIES - STEEL AND HEAT RESISTING ALLOYS - WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PART 004: WIRE |
|
SAE AMS 5339 : 2017
|
STEEL, MARAGING, INVESTMENT CASTINGS, 17NI - 10CO - 4.6MO - 0.30TI - 0.06AL, VACUUM MELTED, HOMOGENIZED, OVERAGED AND SOLUTION HEAT TREATED |
|
SAE AMS 5920 : 2013
|
COBALT-NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, ROUND BARS 19CR - 36CO - 25NI - 7.0MO - 0.50CB (NB) - 2.9TI - 0.20AL - 9.0FE VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED SOLUTION HEAT TREATED, WORK STRENGTHENED AND AGED, MODIFIED STRENGTH |
|
SAE AMS 6931 : 2017
|
TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, ANNEALED |
|
SAE AMS 6472 : 2014
|
STEEL, BARS AND FORGINGS, NITRIDING 1.6CR - 0.35MO - 1.1AL (0.38 - 0.43C) (135 MOD) HARDENED AND TEMPERED, 112 KSI (772 MPA) TENSILE STRENGTH |
|
SAE AS 7109/7 : 2017
|
NADCAP REQUIREMENTS FOR HEAT TREATING FOR SUPPLIERS OF COATINGS |
|
SAE AMS 4934 : 2015
|
TITANIUM ALLOY, EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
|
SAE AMS 2403 : 2015
|
PLATING, NICKEL, GENERAL PURPOSE |
|
SAE AMS 4984F : 2015
|
TITANIUM ALLOY FORGINGS, 10V - 2FE - 3AL, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED AND AGED, 173 KSI (1193 MPA) TENSILE STRENGTH |
|
SAE MA 3377 : 2018
|
BOLTS AND SCREWS, NICKEL ALLOY UNS N07718, TENSILE STRENGTH 1275 MPA PROCUREMENT SPECIFICATION, METRIC |