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SAE AMS 2750 : 2012

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

PYROMETRY

Superseded date

07-02-2020

Published date

01-01-2012

1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGEMENT
7. REJECTIONS
8. NOTES

Describes pyrometric requirements for thermal processing equipment used for heat treatment.

Committee
AMS-B
DocumentType
Standard
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

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<br>
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 AMS2771F: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

ASTM E 230 : 2003 Standard Specification and Temperature-Electromotive Force (EMF) Tables for Standardized Thermocouples
ASTM E 220 : 2013 : REDLINE Standard Test Method for Calibration of Thermocouples By Comparison Techniques

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