SAE AMS2750E
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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Superseded date
02-07-2020
Superseded by
Published date
01-01-2012
Publisher
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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
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| DocumentType |
Standard
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| SAE AMS4901T | 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 AMS2411H | 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 AMS4916L | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| SAE AS7237 | 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 AMS5895E | 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 AMS2762C | 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 AMS4511A | 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 AMS5843G | 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 AMS6327L | 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 AMS4928W | TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
| SAE AMS5711E | 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 AMS2759/7B | CARBURIZING AND HEAT TREATMENT OF CARBURIZING GRADE STEEL PARTS |
| SAE AMS4905F | TITANIUM ALLOY, DAMAGE-TOLERANT GRADE PLATE, 6AL - 4V, BETA ANNEALED |
| SAE AS4877F | 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 AMS4990C | 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 AMS4979J | 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 AMS5663N | 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 AMS6527F | STEEL, BARS AND FORGINGS, 2.0CR - 10NI - 14CO - 1.0MO (0.15 - 0.19C), VACUUM MELTED, NORMALIZED AND OVERAGED |
| SAE AMS5223F | IRON-NICKEL ALLOY, STRIP, 49Fe 5.3Cr 42Ni 2.5Ti 0.55Al, SOLUTION HEAT TREATED, COLD ROLLED, 10% REDUCTION |
| SAE AMS4970K | TITANIUM ALLOY BARS, WIRE, AND FORGINGS 7AL - 4MO SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS2412K | PLATING, SILVER, COPPER STRIKE, LOW BAKE |
| SAE AS 7452 : 2014 | BOLTS AND SCREWS, STEEL, LOW ALLOY HEAT TREATED, ROLL THREADED |
| SAE MA3378D | 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 AMS6433G | 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 AMS4362G | 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 AMS5629H | 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 AMS5704K | 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 AS7466E | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, FATIGUE RATED, PROCUREMENT SPECIFICATION |
| SAE AMS4965L | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS5622F | 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 AMS5655F | 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 AMS5703E | 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 AMS4304B | 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 AMS4921N | 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 AMS5834D | 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 AMS5842G | 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 AMS4914F | TITANIUM ALLOY COLD ROLLED SHEET AND STRIP, 15V - 3AL - 3CR - 3SN, SOLUTION HEAT TREATED |
| SAE AMS4907K | 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 MAM4911B | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4V, ANNEALED |
| AWS C3.4M/C3.4 : 2016 | SPECIFICATION FOR TORCH BRAZING |
| SAE AMS4935L | TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, ANNEALED, BETA PROCESSED |
| SAE AMS5771F | 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 AMS5862M | STEEL, CORROSION-RESISTANT, SHEET, STRIP, AND PLATE, 15CR - 4.5NI - 0.30CB (NB) - 3.5CU, CONSUMABLE ELECTRODE REMELTED, SOLUTION HEAT TREATED, PRECIPITATION-HARDENABLE |
| SAE AMS6949 | 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 AMS4994A | 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 AMS5589F | 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 AS7102B | 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 AMS4898D | 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 AMS5643V | 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 AMS5667N | 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 AMS2769B | 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 AMS5713K | 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 AMS5879D | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND FOIL, 62NI - 21.5CR - 9.0MO - 3.7CB (NB), COLD ROLLED AND ANNEALED |
| SAE AMS5582F | 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 AMSH81200D | 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 AMS5709H | 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 AMS2417J | PLATING, ZINC-NICKEL ALLOY |
| SAE AMS4981H | TITANIUM ALLOY BARS, WIRE, AND FORGINGS, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS6906B | TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION HEAT TREATED AND AGED |
| SAE AMS5383E | 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 AMS5853C | 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 AMS5604J | STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 16.5CR - 4.0NI - 4.0CU - 0.30CB, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS4944L | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3.0AL - 2.5V COLD WORKED, STRESS RELIEVED |
| SAE AMS7725E | 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 AMS5701E | 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 AMS5536N | 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 AMS5706M | 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 AMS4911P | 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 AMS4534C | COPPER-BERYLLIUM ALLOY, BARS AND RODS 98CU - 1.9BE SOLUTION HEAT TREATED, COLD WORKED, AND PRECIPITATION HEAT TREATED (TH04, FORMERLY HT) |
| SAE AMS2759E | HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS |
| SAE AMS4975N | TITANIUM ALLOY, BARS, WIRE, AND RINGS, 6.0AL - 2.0SN - 4.0ZR - 2.0MO - 0.08SI, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS5525J | 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 AMS2759/5D | HEAT TREATMENT, MARTENSITIC CORROSION-RESISTANT STEEL PARTS |
| SAE AMS5894D | 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 AMS4909K | 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 AMS5225F | 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 AS7108C | 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 AMS4919H | 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 AMS5726E | 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 AMS4937D | 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 AMS5891B | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 60NI - 22CR - 2.0MO - 14W - 0.35AL - 0.03LA, ANNEALED |
| SAE AMS4871H | 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 AMS6325K | 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 AMS2774E | 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 AMS6520E | 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 AMS4976K | TITANIUM ALLOY, FORGINGS, 6.0AL - 2.0SN - 4.0ZR - 2.0MO - 08SI, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS2759/6B | 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 AS7459C | BOLTS AND SCREWS, STEEL UNS K14675 TENSILE STRENGTH 195 KSI FATIGUE AND STRESS-RUPTURE RATED PROCUREMENT SPECIFICATION |
| SAE AMS4417C | CASTINGS, SAND, MAGNESIUM ALLOY, 1.5AG - 2.1DI - 0.08CU - 0.70ZR (EQ21A - T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS5772E | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED |
| SAE AMS4958E | TITANIUM ALLOY BARS AND RODS, 3AL - 8V - 6CR - 4MO - 4ZR, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED AND CENTERLESS GROUND OR PEELED AND POLISHED |
| SAE AMS4917J | 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 AMS2685F | 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 AMS2419D | 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 AMS4972H | TITANIUM ALLOY BARS, WIRE, AND RINGS, 8AL - 1MO - 1V, SOLUTION HEAT TREATED AND STABILIZED |
| SAE AMS5583E | 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 AMS2759/4C | HEAT TREATMENT, AUSTENITIC CORROSION-RESISTANT STEEL PARTS |
| API 20B : 2013 | OPEN DIE SHAPED FORGINGS FOR USE IN THE PETROLEUM AND NATURAL GAS INDUSTRY |
| SAE AMS5844H | 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 AS7471H | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07001 TENSILE STRENGTH 165 KSI, CORROSION AND HEAT RESISTANT, PROCUREMENT SPECIFICATION |
| SAE AMS4942G | 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 AS7461D | 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 AMS6532F | STEEL, BARS AND FORGINGS, 3.1CR - 11.5NI - 13.5CO - 1.2MO (0.21 - 0.25C) VACUUM MELTED, NORMALIZED AND OVERAGED, PRECIPITATION HARDENABLE |
| SAE AMS6478B | 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 AMS4973H | 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 AMS6439E | 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 AMS5668J | 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 AMSQQP416E | PLATING, CADMIUM (ELECTRODEPOSITED) |
| API 6D RUSSIAN : 2014 | SPECIFICATION FOR PIPELINE VALVES |
| SAE AMS4232C | 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 AMS5744E | 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 AMS2759/1E | 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 AMS2773E | 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 AMS6512H | 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 AMS5671G | 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 AMS4926N | TITANIUM ALLOY, BARS, WIRE, AND RINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
| SAE AMS5659S | 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 AMS2757B | 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 AMS5708L | 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 AMS4920F | 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 AS7109/5B | NAPCAP REQUIREMENTS FOR COATING EVALUATION LABORATORY PRACTICES |
| SAE AMS2771F | HEAT TREATMENT OF ALUMINUM ALLOY CASTINGS |
| SAE AMS5884D | 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 AMS4303C | 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 AMS5368D | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS 15CR - 4.0NI - 2.3MO - 0.09N SOLUTION HEAT TREATED |
| SAE AMS4915M | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1V - 1MO SINGLE ANNEALED |
| SAE AMS4897D | 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 AMS5608G | 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 AMS5759M | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGING STOCK, FORGINGS, AND RINGS 52CO - 20CR - 10NI - 15W |
| SAE AS7475D | BOLTS, COBALT-CHROMIUM-NICKEL ALLOY, UNS R30159, TENSILE STRENGTH 260 KSI, PROCUREMENT SPECIFICATION |
| SAE AMS4933F | 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 AMS6519D | STEEL, MARAGING, BARS, FORGINGS, TUBING, AND RINGS 19NI - 3.0MO - 1.4TI - 0.10AL PREMIUM AIRCRAFT QUALITY DOUBLE VACUUM MELTED, ANNEALED |
| SAE AMS6525E | 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 AS7109/3B | NADCAP REQUIREMENTS FOR DIFFUSION COATING PROCESSES |
| SAE AMS4918N | 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 AMS5662N | 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 AMS4535D | 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 AMS4442G | 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 AMS5707N | 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 AMS5833D | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, ROUND WIRE 20CR - 15NI - 40CO - 7.0MO - 16FE SOLUTION HEAT TREATED AND COLD DRAWN |
| SAE AMS6543F | 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 AS7467B | BOLTS AND SCREWS, NICKEL ALLOY, UNS N07718, TENSILE STRENGTH 185 KSI, STRESS RUPTURE RATED, PROCUREMENT SPECIFICATION |
| SAE AMS5768L | 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 AMSQQN290C | 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 AMS5876E | 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 AMS5763E | STEEL, CORROSION RESISTANT BARS, FORGINGS, TUBING, AND RINGS, 15CR - 6.5NI - 0.75MO - 0.50CB (NB) - 1.5CU, SOLUTION HEAT TREATED |
| SAE AMS2801B | HEAT TREATMENT OF TITANIUM ALLOY PARTS |
| SAE AMS 2428 : 2017 | PLATING, COBALT-PHOSPHORUS, NANOCRYSTALLINE |
| SAE AMS4941G | 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 AMS4910R | 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 AMS5670F | 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 AMS4999A | 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 AMS7735E | 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 AMS4250B | ALUMINUM ALLOY, PLATE - 8.1ZN - 2.3MG - 1.0CU - ZR (7449-T7651) SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS6526H | 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 AS7468B | 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 MAM5706C | 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 MAM4427A | MAGNESIUM ALLOY SAND CASTINGS 4.0Y - 2.3ND - 0.7ZR (WE43A - T6) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS4943K | TITANIUM ALLOY, HYDRAULIC, SEAMLESS TUBING, 3.0AL - 2.5V, ANNEALED |
| SAE AMS6522D | STEEL PLATE 2.0CR - 10NI - 14CO - 1.0MO (0.13 - 0.17C) VACUUM MELTED, NORMALIZED, AND OVERAGED |
| SAE AMS4352J | 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 AMS5922B | 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 AMS4967L | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
| SAE AMS5360F | 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 AMS4427C | 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 AMS4978H | TITANIUM ALLOY BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS5660L | 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 AMS5858D | 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 AMS4963D | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL - 4.0V, ANNEALED, HEAT TREATABLE, MODIFIED STRENGTH |
| SAE AS7470C | 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 AMS2423E | 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 AMS5712K | 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 AMS4991E | TITANIUM ALLOY CASTINGS, INVESTMENT 6AL - 4V HOT ISOSTATIC PRESSED, ANNEAL OPTIONAL |
| SAE AMS5773E | 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 AMS6317K | STEEL BARS AND FORGINGS, 1.8NI - 0.25MO (0.38 - 0.43C) (4640), HEAT TREATED, 125 KSI (862 MPA) TENSILE STRENGTH |
| SAE AMS6514J | 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 AMS4533D | COPPER-BERYLLIUM ALLOY, BARS AND RODS, 98CU - 1.9BE, SOLUTION AND PRECIPITATION HEAT TREATED (TF00, FORMERLY AT) |
| SAE AMS4924H | TITANIUM ALLOY BARS, FORGINGS, AND RINGS-15, 5AL - 2.5SN, EXTRA LOW INTERSTITIAL, ANNEALED |
| SAE AMS2759/2F | HEAT TREATMENT OF LOW-ALLOY STEEL PARTS MINIMUM TENSILE STRENGTH 220 KSI (1517 MPA) AND HIGHER |
| SAE AMS4957F | 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 AMSH6088C | Heat Treatment of Aluminum Alloys |
| SAE AMS4900P | 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 AMS5859D | 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 AMS4902K | TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY-PURE, ANNEALED 40.0 KSI (276 MPA) YIELD STRENGTH |
| SAE AMS5661F | 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 AMS4930H | 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 AMS6523H | 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 AMS4950D | 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 AMS6257F | 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 AMS4650M | COPPER-BERYLLIUM ALLOY, BARS, RODS, SHAPES, AND FORGINGS 98CU - 1.9BE SOLUTION HEAT TREATED TB00 (A) |
| SAE AMS2376E | 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 AMS4945F | 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 AMS5339G | 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 AMS6472F | 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 AS7109/7B | NADCAP REQUIREMENTS FOR HEAT TREATING FOR SUPPLIERS OF COATINGS |
| SAE AMS4934G | TITANIUM ALLOY, EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS2403M | PLATING, NICKEL, GENERAL PURPOSE |
| SAE AMS4984F | TITANIUM ALLOY FORGINGS, 10V - 2FE - 3AL, CONSUMABLE ELECTRODE MELTED, SOLUTION HEAT TREATED AND AGED, 173 KSI (1193 MPA) TENSILE STRENGTH |
| SAE MA3377C | BOLTS AND SCREWS, NICKEL ALLOY UNS N07718, TENSILE STRENGTH 1275 MPA PROCUREMENT SPECIFICATION, METRIC |
| SAE AMS5940D | 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 |
| SAE AMS2429E | Plating, Bronze, Nitriding Stop-off, 90Cu - 10Sn<br> |
| SAE AMS4938A | Forgings, Titanium Alloys Heat-Treated, Finished-Part Properties: Short-Traverse Tensile, Fracture Toughness, and Longitudinal Time-Dependent-Tension |
| SAE AMS2416M | Plating, Nickel-Cadmium Diffused |
| SAE AMS5922C | Steel, Corrosion-Resistant, Bars, and Forgings, 10Cr - 5.5Ni - 14Co - 2Mo - 1W (0.19-0.23C), Vacuum Induction Melted, Vacuum Arc Remelted, Normalized, Annealed<br> |
| SAE AMS5744F | Steel, Corrosion and Heat-Resistant, Bars and Forgings, 15.5Cr - 4.5Ni - 2.9Mo - 0.10N, Consumable Electrode Remelted, Heat Treated, 170 ksi (1172 MPa) Tensile Strength AMS5744F<br> |
| SAE AMS4990D | Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated and Aged |
| API SPEC 6D:2014+ERR 2:2014 | Specification for Pipeline and Piping Valves<br> |
| SAE AMS6949A | Titanium Alloy, Sheet and Strip 4Al - 2.5V - 1.5Fe Electron Beam Single Melted. Annealed |
| SAE AMS6940B : 2019 | Titanium Alloy Bars, Forgings and Forging Stock, 3.0Al - 2.5V, Annealed<br> |
| SAE AMS4957G | Titanium Alloy, Round Bar and Wire 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Cold Drawn |
| SAE AMS6906C | Titanium Alloy Bars, Forgings, and Forging Stock, 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo, Solution Heat Treated and Aged |
| API SPEC 19LH:2019 | Liner Hanger Equipment |
| SAE AMS5708M | 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 °F (1079 °C) Solution Heat Treated |
| 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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