SAE ARP 1917 : 2002
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
CLARIFICATION OF TERMS USED IN AEROSPACE METALS SPECIFICATIONS
Superseded date
03-01-2016
Published date
01-01-2002
Publisher
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE AMS 4966 : 2017 | TITANIUM ALLOY, FORGINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
| SAE AMS 5697 : 2018 | STEEL, CORROSION-RESISTANT, WIRE, 19CR - 9.5NI (304), SOLUTION HEAT TREATED |
| 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 4916L : 2017 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 8AL - 1MO - 1V DUPLEX ANNEALED |
| SAE AMS 6276 : 2016 | STEEL, BARS, FORGINGS, AND TUBING, 0.50CR - 0.55NI - 0.20MO (0.18 - 0.23C) (SAE 8620), CONSUMABLE ELECTRODE VACUUM REMELTED |
| SAE AMS 3050/3 : 2017 | PERFORMANCE SPECIFICATION ANTI-SEIZE THREAD COMPOUND, HIGH TEMPERATURE - NICKEL ONLY |
| SAE AMS6450K : 2017 | STEEL, SPRING WIRE 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) ANNEALED AND COLD DRAWN |
| SAE AMS 4466 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD, 4.4CU - 1.5MG - 0.60MN (ALCLAD 2024, -T361 SHEET & PLATE), SOLUTION HEAT TREATED, 6% COLD WORKED AND NATURALLY AGED |
| SAE AMS 4405 : 2012 | ALUMINUM ALLOY, ALCLAD SHEET (6156-T4), 1.0SI - 0.90CU - 0.60MN - 0.90MG, SOLUTION HEAT TREATED AND NATURALLY AGED |
| SAE AMS 4332 : 2012 | ALUMINUM ALLOY, EXTRUDED PROFILES (7349-T76511) 8.1ZN - 1.7CU - 2.2MG - 0.16ZR SOLUTION HEAT TREATED, STRESS-RELIEVED, AND OVERAGED |
| SAE AMS 3415 : 2017 | FLUX, ALUMINUM DIP BRAZING 1030 DEGREES F (554 DEGREES C) OR LOWER LIQUIDUS |
| SAE AMS 5866 : 2016 | STEEL, CORROSION-RESISTANT, FLAT WIRE, 18CR - 9.0NI (302), SPRING TEMPER |
| SAE AMS 4992 : 2014 | CASTING, STRUCTURAL INVESTMENT, TITANIUM ALLOY 6AL - 4V HOT ISOSTATICALLY PRESSED |
| 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 4905 : 2017 | TITANIUM ALLOY, DAMAGE-TOLERANT GRADE PLATE, 6AL - 4V, BETA ANNEALED |
| SAE AMS 5553 : 2018 | NICKEL, SHEET AND STRIP, LOW (0.02 MAX) CARBON, ANNEALED |
| SAE AMS 4044 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, 5.6ZN - 2.5MG - 1.6CU - 0.23CR, ANNEALED (7075-O), OR WHEN SPECIFIED, 'AS FABRICATED' (7075-F) |
| SAE AMS 6409E : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) SPECIAL AIRCRAFT QUALITY CLEANLINESS, NORMALIZED AND TEMPERED |
| SAE AMS 5336 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.25 - 0.35C) (4130 MOD) NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS 6330 : 2017 | STEEL BARS, FORGINGS, AND TUBING, 0.65CR - 1.25NI (0.33 - 0.38C) |
| SAE AMS 4245 : 2017 | ALUMINUM ALLOY, WELDING WIRE, 5.0SI - 1.2CU - 0.50MG (C355.0) |
| SAE AMS 1428/2 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN (PSEUDOPLASTIC), SAE TYPES 2, 3, AND 4 NON-GLYCOL BASED |
| SAE AMS 3050/5 : 2017 | PERFORMANCE SPECIFICATION ANTI-SEIZE THREAD COMPOUND, HIGH TEMPERATURE - PTFE ONLY |
| SAE AMS 4979J : 2017 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, SOLUTION AND PRECIPITATION HEAT TREATED |
| 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 AMS6328N : 2017 | STEEL, BARS, FORGINGS, AND TUBING, 0.50CR - 0.55NI - 0.25MO (0.48 TO 0.53C) (SAE 8750) |
| SAE AMS 6434 : 2016 | STEEL, SHEET, STRIP, AND PLATE, 0.78CR - 1.8NI - 0.35MO - 0.20V (0.33 - 0.38C) (4335 MOD) |
| SAE AMS 5647 : 2017 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 19CR - 9.5NI, SOLUTION HEAT TREATED |
| SAE AMS 6274 : 2016 | STEEL BARS, FORGINGS AND TUBING, 0.50CR - 0.55NI - 0.20MO (0.18 - 0.23C) (SAE 8620) |
| SAE AMS 4416 : 2017 | ALUMINUM ALLOY, EXTRUDED PROFILES (2196-T8511) 2.9CU - 1.7LI - 0.4MG - 0.4AG - 0.10ZR SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING AND ARTIFICIALLY AGED |
| SAE AMS 4276 : 2018 | ALUMINUM ALLOY, SHEET - 4.4CU - 1.5MG - 0.60MN (2024-O) ANNEALED, FINE GRAINED |
| SAE AMS 4544 H: 2017 | NICKEL-COPPER ALLOY, CORROSION RESISTANT, SHEET, STRIP, AND PLATE 67NI - 30CU, ANNEALED |
| SAE AMS 4473 : 2017 | ALUMINUM ALLOY PLATE (2624-T39), 4.1CU - 1.4MG - 0.6MN, SOLUTION HEAT TREATED, COLD WORKED AND NATURALLY AGED |
| SAE AMS 5826 : 2017 | STEEL, CORROSION AND HEAT-RESISTANT, WELDING WIRE 15CR - 5.1NI - 0.30CB(NB) - 3.2CU |
| SAE AMS 4462 : 2018 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD, 4.4CU - 1.5MG - 0.60MN (ALCLAD 2024, -T3 SHEET, -T351 PLATE), SOLUTION HEAT TREATED, COLD WORKED AND NATURALLY AGED |
| SAE AMS 4015 : 2018 | ALUMINUM ALLOY, SHEET AND PLATE 2.5MG - 0.25CR (5052-O) ANNEALED |
| SAE AMS 4365 : 2017 | ALUMINUM ALLOY, PLATE, 7.9ZN - 1.2CU - 2.1MG - 0.10ZR (7097-T7651) SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 4345 : 2012 | ALUMINUM ALLOY, EXTRUSIONS - 6.4ZN - 2.4MG - 2.2CU - 0.12ZR (7150-T77511) SOLUTION HEAT TREATED, STRESS-RELIEVED, STRAIGHTENED, AND OVERAGED |
| SAE AMS 7002 : 2018 | PROCESS REQUIREMENTS FOR PRODUCTION OF METAL POWDER FEEDSTOCK FOR USE IN ADDITIVE MANUFACTURING OF AEROSPACE PARTS |
| SAE AMS 5517 : 2010 | STEEL, CORROSION RESISTANT, SHEET AND STRIP, 18CR - 8NI (301) COLD ROLLED, 125 KSI (862 MPA) TENSILE STRENGTH |
| SAE AMS 3050/9 : 2017 | PERFORMANCE SPECIFICATION ANTI-SEIZE THREAD COMPOUND, HIGH TEMPERATURE - 'GRAPHITE+CALCIUM FLUORIDE' ONLY |
| SAE AMS 4921 : 2016 | TITANIUM BARS, WIRE, FORGINGS, AND RINGS COMMERCIALLY PURE, 70 KSI (483 MPA) YIELD STRENGTH |
| SAE AMS 1424/1 : 2016 | DEICING/ANTI-ICING FLUID, AIRCRAFT SAE TYPE 1 GLYCOL (CONVENTIONAL AND NON-CONVENTIONAL) BASED |
| SAE AMS 5350 : 2017 | STEEL, CORROSION AND MODERATE HEAT-RESISTANT, INVESTMENT CASTINGS, 12.5CR (410), HARDENED AND TEMPERED |
| SAE AMS 4374 : 2016 | ALUMINUM ALLOY, EXTRUDED PROFILES, 8.9ZN - 2.2CU - 2.2MG - 0.15ZR (7136-T73511), SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING, STRAIGHTENED, AND OVERAGED |
| SAE AMS 6302K : 2017 | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.65SI - 1.25CR - 0.50MO - 0.25V (0.28 - 0.33C) |
| 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 4344 : 2011 | ALUMINUM ALLOY, EXTRUSIONS, 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7175-T73511), SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING, STRAIGHTENED, AND OVERAGED |
| SAE AMS 5402 : 2004 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS 62NI - 21.5CR - 9.0MO - 3.6CB (NB) AS CAST |
| SAE AMS 4935 : 2017 | TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, ANNEALED, BETA PROCESSED |
| SAE AMS 4049 : 2016 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 5.6ZN - 2.5MG - 1.6CU - 0.23CR (ALCLAD 7075; -T6 SHEET - T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4601 : 2017 | Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked and Naturally Aged (2219 -T31/-T351) |
| 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 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 5916 : 2017 | ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 35FE - 24CR - 37NI - 0.65CB(NB) - 0.2N, ANNEALED |
| SAE AMS 4350 : 2017 | MAGNESIUM ALLOY, EXTRUSIONS 6.5A1 - 0.95ZN (AZ61A-F) AS EXTRUDED |
| SAE AMS 4357 : 2016 | ALUMINUM ALLOY, DIE FORGINGS 3.5CU - 1.0LI - 0.04MG - 0.35MN - 0.45AG - 0.12ZR (2050-T852) SOLUTION HEAT TREATED, COLD WORKED AND ARTIFICIALLY AGED |
| SAE AMS 3920 : 2014 | ACCEPTANCE CRITERIA, ADHESIVE-BONDED METAL-FACED SANDWICH STRUCTURES |
| SAE AMS 5631 : 2018 | STEEL, CORROSION-RESISTANT, BARS AND FORGINGS, 17CR (0.60 - 0.75C) (440A) |
| SAE AMS 6303 : 2018 | STEEL BARS AND FORGINGS, LOW ALLOY, HEAT-RESISTANT, 0.65SI - 1.25CR - 0.50MO - 0.85V (0.25 - 0.30C) |
| SAE AMS 6946 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 4AL - 2.5V - 1.5FE, ANNEALED |
| SAE AMS 4959 : 2017 | TITANIUM ALLOY WIRE 13.5V - 11CR - 3AL SPRING TEMPER |
| SAE AMS 6528 : 2017 | STEEL, BARS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), SPECIAL AIRCRAFT QUALITY CLEANLINESS, NORMALIZED |
| SAE AMS 3379 : 2013(R2018) | SEALING COMPOUND, POLYSULFIDE RUBBER PREFORMED STRIPS FOR SEALING REMOVABLE DOORS, SKINS, AND PANELS |
| 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 |
| SAE AMS 4035 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024-0) ANNEALED; OR WHEN SPECIFIED, 'AS FABRICATED' (2024-F) |
| SAE AMS 4472 : 2017 | ALUMINUM ALLOY, PLATE, 4.0CU - 1.0LI - 0.40MG - 0.35AG - 0.13ZR (2195-T34), SOLUTION HEAT TREATED AND STRESS RELIEVED |
| SAE AMS 4909 : 2016 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN, EXTRA LOW INTERSTITIAL ANNEALED |
| SAE AMS 4249B : 2012 (R2018) | ALUMINUM ALLOY CASTINGS 7.0SI - 0.58MG - 0.15TI - 0.06BE (D357.0-T6) SOLUTION AND PRECIPITATION HEAT TREATED (REQUIRING FATIGUE AND FRACTURE TOUGHNESS TESTING) |
| SAE AMS 5780 : 2018 | STEEL, CORROSION AND HEAT-RESISTANT, WELDING WIRE, 15.5CR - 4.5NI - 2.9MO - 0.10N |
| SAE AMS 6280 : 2017 | STEEL BARS, FORGINGS, AND RINGS, 0.50CR - 0.55NI - 0.20MO (0.28 - 0.33C) (SAE 8630) |
| SAE AMS 2434 : 2017 | PLATING, TIN-ZINC ALLOY |
| SAE AMS 4315 : 2017 | ALUMINUM ALLOY SHEET AND PLATE, 5.6ZN - 2.5MG - 1.6CU - 0.23CR, 7075: (-T76 SHEET, -T7651 PLATE), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 6475 : 2013 | STEEL, NITRIDING, BARS, FORGINGS, AND TUBING, 1.1CR - 3.5NI - 0.25MO - 1.2AL (0.21 - 0.26C) |
| SAE AMS 6953 : 2018 | TITANIUM ALLOY SHEET, 6AL - 4SN - 3NB - 0.5MO - 0.3SI, DUPLEX ANNEALED |
| SAE AMS 4477 : 2017 | ALUMINUM ALLOY, COILED SHEET, 4.4CU - 1.5MG - 0.60MN (2024-T4), SOLUTION TREATED |
| SAE AMS 7875 : 2017 | POWDER, CHROMIUM CARBIDE PLUS NICKEL-CHROMIUM ALLOY, 75CR[2]C[3] + 25 (80NI - 20CR ALLOY) |
| SAE AMS 4256 : 2018 | ALUMINUM ALLOY, CLAD TWO SIDES SHEET - 0.6MG - 0.35SI - 0.28CU (NO. 22 BRAZING SHEET) AS FABRICATED |
| SAE AMS 6408 : 2018 | STEEL, HOTWORK TOOL, BARS AND FORGINGS, 5.25CR - 1.5MO - 1.0V (0.35-0.45C) (H-13), ELECTROSLAG REMELTED (ESR) OR CONSUMABLE ELECTRODE VACUUM ARC REMELTED (VAR), ANNEALED |
| SAE AMS 4269 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN; (2024-T361), SOLUTION HEAT TREATED AND COLD WORKED |
| SAE AMS 4341 : 2011 | ALUMINUM ALLOY, EXTRUSIONS, 6.2ZN - 2.3CU - 2.2MG - 0.12ZR (7050-T73511), SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING, STRAIGHTENED, AND OVERAGED |
| SAE AMS 6352 : 2013 | STEEL SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135) |
| 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 |
| SAE AMS 5824F : 2017 | STEEL, CORROSION-RESISTANT, WELDING WIRE 17CR - 7.1NI - 1.0AL |
| SAE AMS 6548 : 2013 | STEEL BARS, FORGINGS, AND TUBING, 1.0CR - 3.2NI - 0.2MO (0.12 - 0.17C), PREMIUM AIRCRAFT-QUALITY, ELECTROSLAG REMELTED OR CONSUMABLE ELECTRODE VACUUM REMELTED |
| SAE AMS 4296 : 2017 | ALUMINUM ALLOY, ALCLAD SHEET AND PLATE 4.3CU - 1.4MG - 0.60MN (ALCLAD 2524-T3) SOLUTION HEAT TREATED AND COLD WORKED |
| 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 2404 : 2018 | PLATING, ELECTROLESS NICKEL |
| SAE AMS 4290 : 2017 | ALUMINUM ALLOY, DIE CASTINGS 9.5SI - 0.50MG (360.0-F), AS CAST |
| SAE AMS 1428/1 : 2017 | Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV Glycol (Conventional and Non-Conventional) Based |
| SAE AMS 5085 : 2017 | STEEL SHEET, STRIP, AND PLATE, 0.48 - 0.55C (SAE 1050) |
| SAE AMS 6551 : 2013 | STEEL BARS, FORGINGS AND TUBING 1.75CR - 4.0NI - 0.5MO - (0.35 - 0.40C) PREMIUM AIRCRAFT QUALITY CONSUMABLE ELECTRODE VACUUM REMELTED |
| 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 2631 : 2017 | ULTRASONIC INSPECTION, TITANIUM AND TITANIUM ALLOY BAR, BILLET AND PLATE |
| 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 4490 : 2017 | Magnesium Alloy Castings, Die 9.0Al - 0.70Zn (AZ91D, Temper F) As Cast |
| SAE AMS 4291 : 2017 | ALUMINUM ALLOY, DIE CASTINGS, 8.5SI - 3.5CU (A380.0-F), AS CAST |
| SAE AMS 2380 : 2017 | APPROVAL AND CONTROL OF PREMIUM-QUALITY TITANIUM ALLOYS |
| SAE AMS 6456 : 2017 | STEEL, WELDING WIRE, 0.80CR - 1.8NI - 0.25MO (0.35 - 0.40C) (SAE 4340 MOD), VACUUM MELTED, ENVIRONMENT-CONTROLLED PACKAGING |
| 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 6547 : 2013 | STEEL BARS, FORGINGS, AND TUBINGS, 1.0CR - 3.2NI - 0.2MO - (0.12 - 0.17C), AIRCRAFT QUALITY |
| SAE AMS 4946 : 2016 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC, 3AL - 2.5V, TEXTURE CONTROLLED, COLD WORKED, STRESS RELIEVED |
| SAE AMS 4892 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, AS CAST |
| SAE AMS 1424 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1 |
| SAE AMS 4617 : 2017 | ALUMINUM ALLOY, EXTRUSIONS, 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7075-T73, 7075-T73511, 7075-T73510), SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING WHEN REQUIRED, AND OVERAGED |
| SAE AMS 6411 : 2018 | STEEL BARS, FORGINGS, AND TUBING, 0.88CR - 1.8NI - 0.42MO - 0.08V (0.28 - 0.33C) (4330 MOD) CONSUMABLE ELECTRODE REMELTED |
| 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 5846 : 2016 | ALLOY, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS, 53NI - 15CR - 18.5CO - 5.0MO - 3.2TI - 4.2AL - 0.03B, DOUBLE VACUUM MELTED SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 4121 : 2017 | ALUMINUM ALLOY BARS, RODS, AND WIRE, ROLLED, DRAWN, OR COLD FINISHED, 4.5CU - 0.85SI - 0.80MN - 0.50MG (2014-T6, -T651), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5532 : 2017 | IRON ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 30FE - 21CR - 20NI - 20CO - 3.0MO - 2.5W - 1.0CB(NB) - 0.15N, SOLUTION HEAT TREATED |
| SAE AMS4675E : 2017 | NICKEL-COPPER ALLOY, CORROSION-RESISTANT, BARS AND FORGINGS, 67NI - 30CU |
| SAE AMS 4048 : 2016 | ALUMINUM ALLOY SHEET AND PLATE, ALCLAD 5.6ZN - 2.5MG - 1.6CU - 0.23CR (ALCLAD 7075-O) ANNEALED OR WHEN SPECIFIED, 'AS FABRICATED' (ALCLAD 7075-F) |
| 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 4616 : 2012 | SILICON BRONZE BARS, RODS, FORGINGS, AND TUBING 92CU - 3.2SI - 2.8ZN - 1.5FE STRESS RELIEVED |
| 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 |
| 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 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 6494 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 1.0CR - 2.50NI - 2.0MO - 1.10SI (0.10 - 0.20C) AIRCRAFT-QUALITY |
| SAE AMS 4464 : 2017 | ALUMINUM ALLOY PLATE (2624-T351) 4.1CU - 1.4MG - 0.6MN, SOLUTION HEAT TREATED, COLD WORKED AND NATURALLY AGED |
| SAE AMS 6360 : 2013 | STEEL TUBING, SEAMLESS, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), NORMALIZED OR STRESS RELIEVED |
| SAE AMS 4268 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN; (2024-T81 SHEET, -T851 PLATE), SOLUTION HEAT TREATED, COLD WORKED AND ARTIFICIALLY AGED |
| SAE AMS 5618 : 2017 | STEEL, CORROSION-RESISTANT, BARS, WIRE, AND FORGINGS, 17CR - 0.52MO (0.95 - 1.20C) (440C), CONSUMABLE ELECTRODE VACUUM MELTED |
| SAE AMS 4329 : 2017 | ALUMINUM ALLOY, PLATE (7085-T7651), 7.5ZN - 1.6CU - 1.5MG - 0.12ZR, SOLUTION HEAT TREATED, STRESS-RELIEVED, AND OVERAGED |
| SAE AMS 5716 : 2016 | IRON-NICKEL ALLOY, HEAT RESISTANT, BARS, WIRE, FORGINGS, AND RINGS, 44FE - 18.5CR - 35.5NI - 1.1SI, SOLUTION HEAT TREATED |
| SAE AMS 4911 : 2018 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| SAE AMS 2355 : 2017 | QUALITY ASSURANCE, SAMPLING AND TESTING, ALUMINUM ALLOYS AND MAGNESIUM ALLOY, WROUGHT PRODUCTS (EXCEPT FORGING STOCK), AND ROLLED, FORGED, OR FLASH WELDED RINGS |
| SAE AMS 2759 : 2014 | HEAT TREATMENT OF STEEL PARTS, GENERAL REQUIREMENTS |
| SAE AMS 6348 : 2013 | STEEL, BARS, 0.95CR - 0.20MO (0.28 TO 0.33C) (SAE 4130), NORMALIZED |
| SAE AMS 4712 : 2017 | COPPER ALLOY, WIRE 65CU - 35ZN ANNEALED (O61) |
| SAE AMS 5504 : 2018 | Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 12.5Cr (410) Annealed |
| SAE AMS 5702 : 2018 | 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, 1750 DEGREES F (954 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 4403 : 2017 | ALUMINUM ALLOY, DIE FORGINGS, 7.5ZN - 1.6CU - 1.5MG - 0.12ZR (7085-T7452), SOLUTION HEAT TREATED, COMPRESSION STRESS-RELIEVED, AND OVERAGED |
| SAE AMS 5808 : 2018 | STEEL, CORROSION AND HEAT-RESISTANT, WELDING WIRE, 19CR - 13NI - 2.5MO, HIGH FERRITE GRADE, TRACE ELEMENT CONTROLLED |
| SAE AMS 4955 : 2016 | TITANIUM ALLOY, WELDING WIRE 8AL - 1MO - 1V |
| SAE AMS 3050/7 : 2017 | Performance Specification Anti-Seize Thread Compound, High Temperature – ‘Copper+Graphite+Aluminum’ Only |
| SAE AMS 4078 : 2011 | ALUMINUM ALLOY SHEET AND PLATE, 5.6ZN - 2.5MG - 1.6CU - 0.23CR, 7075: (-T73 SHEET, -T7351 PLATE), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 4939C : 2017 | TITANIUM ALLOY SHEET, STRIP, AND PLATE, 3AL - 8V - 6CR - 4MO - 4ZR, SOLUTION HEAT TREATED |
| SAE AMS 4458 : 2016 | ALUMINUM ALLOY, PLATE (2.7 CU - 1.8 LI - 0.7 ZN) 2099-T86, SOLUTION HEAT TREATED, COLD WORKED AND ARTIFICIALLY AGED |
| SAE AMS 6308 : 2012 | STEEL, BARS AND FORGINGS, 0.90SI - 1.0CR - 2.0NI - 3.2MO - 2.0CU - 0.10V (0.07 - 0.13C), VACUUM ARC OR ELECTROSLAG REMELTED |
| SAE AMS 6304 : 2016 | LOW-ALLOY STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.95CR - 0.55MO - 0.30V (0.40 - 0.50C) |
| SAE AMS 6320 : 2017 | STEEL BARS, FORGINGS, AND RINGS 0.50CR - 0.55NI - 0.25MO (0.33 - 0.38C) (8735) |
| SAE AMS 6484 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) NORMALIZED AND TEMPERED |
| SAE AMS 4978 : 2018 | TITANIUM ALLOY BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED |
| SAE AMS 5930 : 2017 | STEEL, CORROSION-RESISTANT, BARS AND FORGINGS 13.0CR - 2.5NI - 5.5CO - 2.0MO - 0.60V (0.05 - 0.09C) VACUUM INDUCTION PLUS VACUUM CONSUMABLE ELECTRODE MELTED |
| SAE AMS 4285 : 2017 | ALUMINUM ALLOY CASTINGS, CENTRIFUGAL, 7.0SI - 0.30MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 6455 : 2016 | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) |
| SAE AMS 4406 : 2018 | Aluminum Alloy, Centrifugal Castings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (709.0-T61) Hot Isostatically Pressed, Solution and Precipitation Heat Treated |
| SAE AMS 4277 : 2018 | ALUMINUM ALLOY, SHEET - 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7075-O) ANNEALED, FINE GRAINED |
| SAE AMS 6951 : 2017 | TITANIUM ALLOY, SHEET 5AL - 4V - 0.75MO - 0.5FE ANNEALED |
| SAE AMS 4339 : 2018 | ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS AND RODS 4.4CU - 1.5MG - 0.60MN (2024-T-851) SOLUTION HEAT TREATED, COLD WORKED, AND ARTIFICIALLY AGED |
| SAE AMS 1428 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4 |
| SAE AMS 4079 : 2017 | ALUMINUM ALLOY, DRAWN, ROUND, SEAMLESS, TUBING, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061-O), CLOSE TOLERANCE, ANNEALED |
| SAE AMS 5898 : 2018 | STEEL, CORROSION RESISTANT, BARS, WIRE, AND FORGINGS, 15.2CR - 1.0MO - 0.40N - (0.28 - 0.34C), CONSUMABLE ELECTRODE MELTED UNDER PRESSURE |
| SAE AMS 6323 : 2017 | STEEL, MECHANICAL TUBING 0.50CR - 0.55NI - 0.25MO (0.38 - 0.43C) (SAE 8740) |
| SAE AMS 4612 : 2017 | BRASS, NAVAL, BARS AND RODS 60.5CU - 38.5ZN - 0.75SN HARD TEMPER (H04) |
| SAE AMS 4193 : 2017 | ALUMINUM ALLOY SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024-T861), SOLUTION HEAT TREATED, COLD WORKED, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5505 : 2018 | STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 12CR (410 MODIFIED), FERRITE CONTROLLED, ANNEALED |
| SAE AMS 4625 : 2016 | PHOSPHOR BRONZE BARS, RODS, AND TUBING, 95CU - 5SN, HARD TEMPER |
| SAE AMS 4094 : 2018 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI ALCLAD 2219-T81 SHEET SOLUTION HEAT TREATED, COLD WORKED, AND PRECIPITATION HEAT TREATED ALCLAD 2219-T851 PLATE SOLUTION HEAT TREATED, STRESS RELIEVED, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5338 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.35 - 0.45C) (4140 MOD), NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS 5046 : 2017 | CARBON STEEL, SHEET, STRIP, AND PLATE, (SAE 1020 AND 1025) |
| SAE AMS 2418 : 2017 | PLATING, COPPER |
| 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 4251 : 2017 | ALUMINUM ALLOY SHEET, 2.7CU - 2.2LI - 0.12ZR (2090-T83), SOLUTION HEAT TREATED, COLD WORKED, AND PRECIPITATION HEAT TREATED |
| SAE AMS 5650 : 2018 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 23CR - 13.5NI (309S), SOLUTION HEAT TREATED |
| SAE AMS 6501 : 2017 | STEEL, MARAGING, WELDING WIRE, 18NI - 8.0CO - 4.9MO - 0.40TI - 0.10AL, VACUUM INDUCTION MELTED, ENVIRONMENT CONTROLLED PACKAGING |
| 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 6539 : 2013 | STEEL BARS, FORGINGS, AND TUBING, 1.7CR - 3.8NI - 0.3MO - (0.32-0.38 C), AIRCRAFT-QUALITY |
| SAE AMS 4045 : 2016 | ALUMINUM ALLOY SHEET AND PLATE 5.6ZN - 2.5MG - 1.6CU - 0.23CR 7075: (-T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED |
| 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 6463 : 2013 | WIRE, STEEL WELDING, 18.5NI - 8.5CO - 5.2MO - 0.72TI - 0.10AL, (MARAGE 300), VACUUM MELTED, ENVIRONMENT CONTROLLED PACKAGING |
| 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 4463 : 2017 | ALUMINUM ALLOY, PLATE (7255-T7751) 8.0ZN - 2.3CU - 2.0MG - 0.12ZR, SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 4917 : 2017 | TITANIUM ALLOY SHEET, STRIP, AND PLATE 13.5V - 11CR - 3.0AL - SOLUTION HEAT TREATED |
| SAE AMS 6415 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
| SAE AMS 4212 : 2016 | Aluminum Alloy Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS 6381 : 2017 | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140) |
| SAE AMS 6414 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) VACUUM CONSUMABLE ELECTRODE REMELTED |
| SAE AMS 2466 : 2018 | HARD ANODIC COATING OF MAGNESIUM ALLOYS |
| SAE AMS 4225 : 2018 | ALUMINUM ALLOY, HEAT-RESISTANT, CASTINGS, 5.0CU - 1.5NI - 0.25MN - 0.25SB - 0.25CO - 0.20TI - 0.20ZR (203.0-T6), SOLUTION HEAT TREATED AND PRECIPITATION HEAT TREATED |
| SAE AMS 4017 : 2018 | ALUMINUM ALLOY SHEET AND PLATE, 2.5MG - 0.25CR, (5052-H34), STRAIN-HARDENED, HALF-HARD, AND STABILIZED |
| SAE AMS 6305 : 2016 | STEEL, HEAT-RESISTANT, BARS, FORGINGS, AND TUBING, 0.95CR - 0.55MO - 0.30V (0.40 - 0.50C), VACUUM ARC REMELTED |
| SAE AMS 5632 : 2018 | STEEL, CORROSION-RESISTANT, BARS, WIRE, AND FORGINGS, 17CR - 0.50MO (0.95 - 1.20C) (440F), FREE-MACHINING, ANNEALED |
| SAE AMS 5635 : 2018 | STEEL, CORROSION-RESISTANT, BARS, WIRE, AND FORGINGS, 18CR - 9NI - 0.21PB (303PB), FREE-MACHINING, SOLUTION HEAT TREATED |
| SAE AMS 2249 : 2017 | CHEMICAL CHECK ANALYSIS LIMITS, TITANIUM AND TITANIUM ALLOYS |
| SAE AMS 4157 : 2018 | ALUMINUM ALLOY EXTRUSIONS, 7.7ZN - 2.4MG - 1.6CU - 0.16CR (7049-T73511), SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 4327 : 2016 | ALUMINUM ALLOY, PLATE (2098-O), 3.5CU - 1.1LI - 0.50MG - 0.40AG - 0.11ZR, ANNEALED |
| SAE AIR 4779 : 2014 | USER'S GUIDE TO AMS SPECIFICATIONS |
| SAE AMS 4942 : 2018 | TITANIUM TUBING, SEAMLESS, ANNEALED, 40.0 KSI (275 MPA) YIELD STRENGTH |
| SAE AMS 4553D : 2017 | BRASS, SEAMLESS, TUBING 85CU - 15ZN ANNEALED (O61) |
| SAE AMS 6277 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 0.50CR - 0.55NI - 0.20MO (0.18 - 0.23C) (SAE 8620), VACUUM ARC OR ELECTROSLAG REMELTED |
| 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 |
| SAE AMS 5585 : 2016 | ALLOY, CORROSION AND HEAT RESISTANT, WELDED TUBING, 32FE - 21CR - 20NI - 20CO - 3MO - 2.5W - 1.0CB (NB) - 0.15N, SOLUTION HEAT TREATED |
| SAE AMS 4993F : 2017 | TITANIUM ALLOY, BLENDED POWDER COMPACTS, SINTERED, 6AL - 4V |
| SAE AMS 5558H : 2016 | STEEL, CORROSION AND HEAT-RESISTANT, WELDED TUBING 18CR - 10.5NI - 0.70CB (NB) (347) THIN WALL SOLUTION HEAT TREATED |
| SAE AMS 6267J: 2016 | STEEL BARS, FORGINGS, AND TUBING, 1.2CR - 3.25NI - 0.12MO (0.07 - 0.13C) (9310), ELECTROSLAG REMELTED OR CONSUMABLE ELECTRODE VACUUM REMELTED |
| SAE AMS 7000 : 2018 | LASER-POWDER BED FUSION (L-PBF) PRODUCED PARTS, NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, 62NI - 21.5CR - 9.0MO - 3.65NB STRESS RELIEVED, HOT ISOSTATIC PRESSED AND SOLUTION ANNEALED |
| SAE AMS 6457E : 2017 | STEEL, WELDING WIRE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), VACUUM MELTED, ENVIRONMENT CONTROLLED PACKAGING |
| SAE AMS 4284 : 2017 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 7.0SI - 0.30MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 2420 : 2017 | PLATING OF ALUMINUM FOR SOLDERABILITY ZINC IMMERSION PRE-TREATMENT PROCESS |
| 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 6255F : 2016 | STEEL BARS, FORGINGS, AND TUBING, 1.1SI - 1.45CR - 1.0MO - 0.08AL (0.16 - 0.22C), DOUBLE VACUUM MELTED |
| NASA HDBK 6025 : 2014 | GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS |
| SAE AMS 4973 : 2016 | TITANIUM ALLOY FORGINGS, 8AL - 1MO - 1V, SOLUTION HEAT TREATED AND STABILIZED |
| 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 |
| SAE AMS 6558 : 2013 | STEEL, BARS, WIRE, AND FORGINGS 10.5MO - 6W - 3.75CR - 2V (1.25 - 1.40C) POWDER METALLURGY PRODUCT HOT ISOSTATICALLY PRESSED |
| SAE AMS 3050/6 : 2017 | Performance Specification Anti-Seize Thread Compound, High Temperature - ‘Nickel+Graphite’ Only |
| SAE AMS 4599 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, 6.3CU - 0.30MN - 0.06TI - 0.10V - 0.18ZR, SOLUTION AND PRECIPITATION HEAT TREATED (2219 -T81/-T851) |
| SAE AMS 4163 : 2017 | ALUMINUM ALLOY, EXTRUSIONS 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI (2219-T3511) SOLUTION HEAT TREATED, STRESS-RELIEVED BY STRETCHING, AND STRAIGHTENED |
| SAE AMS 6950 : 2017 | TITANIUM ALLOY BARS, FORGINGS, AND FORGING STOCK 4AL - 2.5V - 1.5 FE SINGLE HEARTH MELTED, ANNEALED |
| SAE AMS 4940 : 2017 | TITANIUM SHEET, STRIP, AND PLATE COMMERCIALLY PURE ANNEALED, 25.0 KSI (172 MPA) YIELD STRENGTH |
| SAE AMS 4342 : 2018 | ALUMINUM ALLOY, EXTRUSIONS, 6.2ZN - 2.3CU - 2.2MG - 0.12ZR (7050-T74511), SOLUTION HEAT TREATED, STRESS RELIEVED, STRAIGHTENED, AND OVERAGED |
| SAE AMS 5596 : 2017 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED, 1775 DEGREES F (968 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 4211 : 2012 | ALUMINUM ALLOY, PLATE, 6.2ZN - 1.9CU - 2.1MG - 0.10ZR (7040-T7451) SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 5597 : 2016 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 52.5NI - 19CR - 3.0MO - 5.1CB (NB) - 0.90TI - 0.50AL - 18FE, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1950 DEGREES F (1066 DEGREES C) SOLUTION HEAT TREATED |
| SAE AMS 6260S : 2016 | STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 3.2NI - 0.12MO (0.07 - 0.13C) (9310) |
| SAE AMS 4194 : 2018 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 4.4CU - 1.5MG - 0.60MN (2024 -T361 SHEET/PLATE WITH 1-1/2% ALCLAD) SOLUTION HEAT TREATED, 6% COLD WORKED AND NATURALLY AGED |
| 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 4633 : 2018 | BRONZE, ALUMINUM SILICON, RODS, BARS, AND FORGINGS 90CU - 7.0AL - 1.8SI DRAWN AND STRESS RELIEVED (HR50) |
| SAE AMS 6430J : 2017 | STEEL, BARS, FORGINGS, TUBING, AND RINGS, 0.75MN - 0.78CR - 1.8NI - 0.35MO - 0.20V (0.32 - 0.38C), (4335 MODIFIED) |
| SAE AMS 6372 : 2017 | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.33 - 0.38C) (SAE 4135) |
| SAE AMS 4206 : 2017 | ALUMINUM ALLOY, PLATE (7055-T7751), 8.0ZN - 2.3CU - 2.0MG - 0.16ZR, SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 4343 : 2012 | ALUMINUM ALLOY, EXTRUSIONS, 7.7ZN - 2.4MG - 1.6CU - 0.16CR, (7149-T73511) SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING, AND OVERAGED |
| SAE AMS 4951 : 2017 | TITANIUM WELDING WIRE COMMERCIALLY PURE ENVIRONMENT CONTROLLED PACKAGING |
| SAE AMS 4730 : 2017 | NICKEL-COPPER ALLOY WIRE, CORROSION-RESISTANT, 67NI - 31CU ANNEALED (400) |
| SAE AMS5659S : 2016 | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu<br> |
| SAE AMS 4954 : 2017 | TITANIUM ALLOY, WELDING WIRE 6AL - 4V |
| SAE AMS 1424/2 : 2016 | DEICING/ANTI-ICING FLUID, AIRCRAFT SAE TYPE 1 NON-GLYCOL BASED |
| SAE AMS 5689 : 2018 | STEEL, CORROSION AND HEAT RESISTANT, WIRE 18CR - 10.5NI - 0.40TI (321) SOLUTION HEAT TREATED |
| SAE AMS 4299 : 2018 | ALUMINUM ALLOY, PLATE (7449-T7951), 8.1ZN - 1.8CU - 2.3MG SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 5664 : 2017 | 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 1950 DEGREES F (1066 DEGREES C) SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 4461 : 2012 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD, 4.4CU - 1.5MG - 0.60MN (ALCLAD 2024-O, SHEET AND PLATE) ANNEALED; OR WHEN SPECIFIED, 'AS FABRICATED' (2024-F) |
| SAE AMS 4956 : 2016 | TITANIUM ALLOY WELDING WIRE, 6AL - 4V, EXTRA LOW INTERSTITIAL, ENVIRONMENT CONTROLLED PACKAGING |
| 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 2545 : 2017 | CONTROLLED PNEUMATIC NEEDLE PEENING, STRAIGHTENING AND FORMING |
| SAE AMS 2771 : 2017 | HEAT TREATMENT OF ALUMINUM ALLOY CASTINGS |
| SAE AMS 4348 : 2018 | CORE, HONEYCOMB, ALUMINUM ALLOY, CORROSION INHIBITED FOR SANDWICH CONSTRUCTION 5052, 350 (177) |
| SAE AMS 4478 : 2018 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD, 4.4CU - 1.5MG - 0.60MN (ALCLAD 2024, -T81 SHEET, -T851 PLATE), SOLUTION HEAT TREATED, COLD WORKED AND ARTIFICIALLY AGED |
| SAE AMS 4558 : 2017 | BRASS, SEAMLESS TUBING, 66.5CU - 31.5ZN - 1.6PB, DRAWN TEMPER (H58) |
| 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 3050/8 : 2017 | Performance Specification Anti-Seize Thread Compound, High Temperature - ‘Graphite+Aluminum’ Only |
| SAE AMS 4779 : 2018 | NICKEL ALLOY, BRAZING FILLER METAL, 94NI - 3.5SI - 1.8B, 1800 DEGREES F (982 DEGREES C) SOLIDUS, 1950 DEGREES F (1066 DEGREES C) LIQUIDUS |
| SAE AMS 5608 : 2016 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 40CO - 22CR - 22NI - 14.5W - 0.07LA, SOLUTION HEAT TREATED |
| SAE AMS 4893 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, SOLUTION TREATED |
| SAE AMS 5694 : 2018 | STEEL, CORROSION AND HEAT RESISTANT, WELDING WIRE, 27CR - 21.5NI |
| SAE AMS 2449 : 2010 | GRINDING OF HVOF SPRAYED TUNGSTEN CARBIDE COATINGS APPLIED TO HIGH STRENGTH STEELS |
| SAE AMS 4189 : 2016 | ALUMINUM ALLOY WELDING WIRE, 4.1SI-0.20 MG (4643) |
| SAE AMS 3050/1 : 2017 | PERFORMANCE SPECIFICATION ANTI-SEIZE THREAD COMPOUND, HIGH TEMPERATURE - COPPER ONLY |
| SAE AMS 5687N : 2018 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, WIRE, 74NI - 15.5CR - 8.0FE, ANNEALED |
| 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 6354 : 2016 | STEEL, SHEET, STRIP, AND PLATE, 0.75SI - 0.62CR - 0.20MO - 0.10ZR (0.10 - 0.17C) |
| SAE AMS4933F : 2017 | TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS 8AL - 1MO - 1V SOLUTION HEAT TREATED AND STABILIZED |
| 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 7001 : 2018 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, POWDER FOR ADDITIVE MANUFACTURING, 62NI - 21.5CR - 9.0MO - 3.65NB |
| 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 AMS4221E : 2016 | ALUMINUM ALLOY, PLATE, 4.4CU - 1.5MG - 0.60MN (2124-T8151) SOLUTION HEAT TREATED, STRESS RELIEVED, AND PRECIPITATION HEAT TREATED |
| SAE AMS 4149 : 2016 | ALUMINUM ALLOY, DIE AND HAND FORGINGS, 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7175-T74), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4375 : 2017 | SHEET AND PLATE, MAGNESIUM ALLOY - 3.0AL - 1.0ZN - 0.20MN (AZ31B-0) ANNEALED AND RECRYSTALLIZED |
| 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 5825 : 2017 | STEEL, CORROSION-RESISTANT, WELDING WIRE 16.4CR - 4.8NI - 0.22CB(NB) - 3.6CU |
| SAE AMS 5540 : 2017 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 74NI - 15.5CR - 8.0FE, ANNEALED |
| SAE AMS 2821 : 2017 | SALTS, HEAT-TREATING (FOR METALS) |
| SAE AMS 4120 : 2018 | ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS, RODS, AND WIRE, 4.4CU - 1.5MG - 0.60MN (2024), SOLUTION HEAT TREATED AND NATURALLY AGED (T4), SOLUTION HEAT TREATED, COLD WORKED, AND NATURALLY AGED (T351) |
| SAE AMS 5917 : 2011 | METAL INJECTION MOLDED NICKEL BASED, ALLOY 718 PARTS, HOT ISOSTATICALLY PRESSED, SOLUTIONED AND AGED |
| SAE AMS 4313 : 2016 | ALUMINUM ALLOY, ROLLED OR FORGED RINGS, 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI (2219-T351, 2219-T352) SOLUTION HEAT TREATED AND MECHANICALLY STRESS RELIEVED |
| SAE AMS 4041 : 2012-07 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 4.4CU - 1.5MG - 0.60MN (2024, -T3 SHEET/-T351 PLATE WITH 1-1/2% ALCLAD) SOLUTION HEAT TREATED, COLD WORKED AND NATURALLY AGED |
| SAE AMS 4475 : 2017 | Aluminum Alloy, Coiled Sheet, Alclad 4.4Cu – 1.5Mg – 0.60Mn (Alclad 2024; -T4 Coiled Sheet) Solution Heat Treated |
| SAE AMS 6529 : 2017 | STEEL, BARS, 0.95CR - 0.20MO (0.38 - 0.43C) (SAE 4140), SPECIAL AIRCRAFT-QUALITY CLEANLINESS, NORMALIZED |
| SAE AMS 6448 : 2013 | STEEL, BARS, FORGINGS AND TUBING 0.95CR - 0.22V (0.48 - 0.53C) (SAE 6150) |
| SAE AMS 5357 : 2017 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 3025 : 2018 | POLYALKYLENE GLYCOL HEAT TREAT QUENCHANT |
| SAE AMS 4467 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 4.4CU 1.5MG 0.60MN (ALCLAD 2024, -T861 SHEET & PLATE) SOLUTION HEAT TREATED, 6% COLD WORKED AND ARTIFICIALLY AGED |
| SAE AMS 2409 : 2016 | PLATING, IMMERSION TIN FOR ALUMINUM ALLOYS |
| SAE AMS 6346 : 2013 | STEEL BARS, 0.95CR - 0.20MO (0.28 TO 0.33C) (SAE 4130), HARDENED AND TEMPERED, 125 KSI (862 MPA) TENSILE STRENGTH |
| SAE AMS 6424 : 2017 | STEEL BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.49 - 0.55C) |
| 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 2428 : 2017 | PLATING, COBALT-PHOSPHORUS, NANOCRYSTALLINE |
| SAE AMS 4941 G : 2017 | TITANIUM TUBING, WELDED, 40 KSI (276 MPA) YIELD STRENGTH |
| SAE AMS 4434 : 2017 | MAGNESIUM ALLOY CASTINGS, SAND, 9.0AL - 2.0ZN (AZ92A-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 6290 : 2013 | STEEL, BARS AND FORGINGS, CARBURIZING, 1.8NI - 0.25MO (0.11 - 0.17C) (SAE 4615) |
| SAE AMS 5718E : 2016 | STEEL, BARS, FORGINGS, TUBING, AND RINGS, CORROSION RESISTANT, 11.8CR - 2.5NI - 1.8MO - 0.33V (0.08 - 0.15C), ANNEALED |
| SAE AMS 4910 : 2017 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE 5AL - 2.5SN ANNEALED |
| 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 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 |
| SAE AMS 6435 : 2017 | STEEL, SHEET, STRIP, AND PLATE, 0.75MN - 0.78CR - 1.8NI - 0.35MO - 0.20V (0.33 - 0.38C) (4335 MOD), VACUUM CONSUMABLE ELECTRODE MELTED, ANNEALED |
| SAE AMS 5506 : 2018 | STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE, 13CR (0.30 - 0.40C) (420), ANNEALED |
| SAE AMS 6560 : 2013 | STEEL BARS, WIRE AND FORGINGS 10CO - 7MO - 6V - 6W - 4CR (2.2 - 2.4C) PREMIUM AIRCRAFT-QUALITY FOR BEARING APPLICATIONS INERT GAS ATOMIZED AND HOT ISOSTATICALLY PRESSED CONSOLIDATED |
| SAE AMS 4402 : 2018 | ALUMINUM ALLOY, EXTRUDED PROFILES (2024-T432), 4.4CU - 1.5MG - 0.6MN, ANNEALED, STRETCH FORMED, SOLUTION HEAT TREATED AND STRESS RELIEVED BY STRETCHING |
| SAE AMS 4359 : 2016 | ALUMINUM ALLOY, EXTRUDED PROFILES (2395-T84), 3.95CU - 1.15LI - 0.3AG - 0.5MG - 0.1ZR, SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING, AND AGED |
| SAE AMS6481D:2017 | STEEL BARS, FORGINGS, AND TUBING, NITRIDING, 3CR - 1MO - 0.2V - (0.29 - 0.36C), PREMIUM AIRCRAFT-QUALITY FOR BEARING APPLICATIONS, DOUBLE VACUUM MELTED |
| SAE AMS 5333 : 2017 | STEEL, INVESTMENT CASTINGS, 0.50CR - 0.55NI - 0.25MO (0.11 - 0.17C) (SAE 8615), NORMALIZED |
| SAE AMS 2259 : 2017 | CHEMICAL CHECK ANALYSIS LIMITS, WROUGHT LOW-ALLOY AND CARBON STEELS |
| SAE AMS 4095 : 2018 | ALUMINUM ALLOY, ALCLAD SHEET AND PLATE 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI ALCLAD 2219-T31; SHEET, SOLUTION HEAT TREATED AND COLD WORKED ALCLAD 2219-T351; PLATE, SOLUTION HEAT TREATED AND STRESS RELIEVED |
| SAE AMS 4040 : 2018 | ALUMINUM ALLOY, SHEET AND PLATE, ALCLAD 4.4CU - 1.5MG - 0.60MN (2024-O WITH 1-1/2% ALCLAD); ANNEALED |
| SAE AMS 7735 : 2018 | ALLOY WIRE, ROUND, 35PD - 30AG - 14CU - 10AU - 10PT - 0.85ZN, SOLUTION HEAT TREATED |
| SAE AMS 4338 : 2007 | ALUMINUM ALLOY, EXTRUSIONS, 4.0CU - 1.3MG - 0.60MN (2026-T3511), SOLUTION HEAT TREATED AND STRESS RELIEVED BY STRETCHING |
| 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 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 AMS 4372 : 2018 | ALUMINUM ALLOY, PLATE, 3.5CU - 1.0LI - 0.40MG - 0.35MN - 0.45AG - 0.12ZR (2050-T34), SOLUTION HEAT TREATED AND STRESS RELIEVED |
| SAE AMS 4970 : 2016 | TITANIUM ALLOY BARS, WIRE, AND FORGINGS 7AL - 4MO SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4574F : 2017 | NICKEL-COPPER ALLOY, CORROSION RESISTANT, TUBING, SEAMLESS 67NI - 31CU ANNEALED |
| SAE AMS 4368 : 2017 | ALUMINUM ALLOY, DISCONTINUOUSLY REINFORCED HOT ISOSTATICALLY PRESSED SHAPES 6061B/SIC/40P (3[MU]M) (T1P) |
| SAE AS 6279 : 2016 | STANDARD PRACTICE FOR PRODUCTION, DISTRIBUTION, AND PROCUREMENT OF METAL STOCK |
| SAE AMS 4352J : 2017 | MAGNESIUM ALLOY, EXTRUSIONS, 5.5ZN - 0.45ZR (ZK60A - T5), PRECIPITATION HEAT TREATED |
| SAE AMS 2647F : 2017 | FLUORESCENT PENETRANT INSPECTION, AIRCRAFT AND ENGINE COMPONENT MAINTENANCE |
| SAE AMS 5639 : 2017 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 19CR - 10NI, SOLUTION HEAT TREATED |
| SAE AMS 4967 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
| SAE AMS 5811 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, WELDING WIRE, 15CR - 30NI - 1.2MO - 2.2TI - 0.25AL - 0.001B - 0.030V (0.01 - 0.03C), VACUUM INDUCTION MELTED, ENVIRONMENT CONTROLLED PACKAGING |
| SAE AMS 4071 : 2017 | ALUMINUM ALLOY, DRAWN, ROUND, SEAMLESS HYDRAULIC TUBING, 2.5MG - 0.25CR (5052-O), ANNEALED |
| SAE AMS 7498 : 2016 | RINGS, FLASH WELDED TITANIUM AND TITANIUM ALLOYS |
| SAE AMS 4971L : 2017 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6AL - 6V - 2SN, ANNEALED, HEAT TREATABLE |
| SAE AMS 5648 : 2016 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 17CR - 12NI - 2.5MO (316), SOLUTION HEAT TREATED |
| SAE AMS 4255 : 2012 | ALUMINUM ALLOY, CLAD ONE SIDE SHEET - 0.6MG - 0.35SI - 0.28CU (NO. 21 BRAZING SHEET) AS FABRICATED |
| SAE AMS 4949 : 2017 | TITANIUM, SHEET, LAMINATED, SURFACE BONDED |
| SAE AMS 4676 : 2017 | NICKEL-COPPER ALLOY, CORROSION-RESISTANT, BARS AND FORGINGS, 66.5NI - 3.0AL - 0.62TI - 28CU, HOT-FINISHED, PRECIPITATION HARDENABLE |
| SAE AMS 5537 : 2017 | COBALT ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, FOIL, AND PLATE, 52CO - 20CR - 10NI - 15W, SOLUTION HEAT TREATED |
| SAE AMS 4002 : 2018 | ALUMINUM ALLOY TUBING, SEAMLESS, DRAWN 1.8CU - 1.0MG - 0.8SI - 0.20CR SOLUTION HEAT TREATED, STRESS-RELIEVED BY STRETCHING, AND AGED (2013-T6511) |
| SAE AMS 4613 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, 6.3CU - 0.30MN - 0.06TI - 0.10V - 0.18ZR, SOLUTION HEAT TREATED, COLD WORKED (8%) AND PRECIPITATION HEAT TREATED (2219 -T87) |
| SAE AMS 4963 : 2016 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL - 4.0V, ANNEALED, HEAT TREATABLE, MODIFIED STRENGTH |
| SAE AMS 3050/4 : 2017 | PERFORMANCE SPECIFICATION ANTI-SEIZE THREAD COMPOUND, HIGH TEMPERATURE - MOLYBDENUM DISULPHIDE; GRAPHITE ONLY |
| 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 4031 : 2017 | ALUMINUM ALLOY, SHEET AND PLATE, 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI (2219-O) ANNEALED OR WHEN SPECIFIED, 'AS FABRICATED' (2219-F) |
| SAE AMS 4085 : 2011 | ALUMINUM ALLOY SHEET, 5.7ZN - 2.2MG - 1.6CU - 0.22CR (7475-T761), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 5599 : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 62NI - 21.5CR - 9.0MO - 3.7 CB (NB), ANNEALED |
| SAE AMS 6495 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 1.0CR - 2.50NI - 2.0MO - 1.10SI (0.10 - 0.20C), PREMIUM AIRCRAFT-QUALITY, ELECTROSLAG REMELTED OR CONSUMABLE ELECTRODE VACUUM REMELTED |
| 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 4407 : 2018 | ALUMINUM ALLOY, PLATE (7056-T7651), 9.1ZN - 1.6CU - 1.9MG, SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 6407 : 2017 | STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 2.0NI - 0.45MO (0.27 - 0.33C) |
| 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 6265 : 2016 | STEEL, BARS, FORGINGS, AND TUBING, 1.2CR - 3.25NI - 0.12MO (0.07 - 0.13C) (9310), VACUUM CONSUMABLE ELECTRODE REMELTED |
| SAE AMS 6349 : 2017 | STEEL BARS, 0.95CR - 0.20MO (0.38 TO 0.43C) (SAE 4140), NORMALIZED |
| SAE AMS 1435 : 2012 | FLUID, GENERIC, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS |
| SAE AMS 6431 : 2017 | STEEL, BARS, FORGINGS, AND TUBING, 1.05CR - 0.55NI - 1.0MO - 0.11V (0.45 - 0.50C) (D6AC), VACUUM CONSUMABLE ELECTRODE REMELTED |
| 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 |
| SAE AMS 6487 : 2016 | STEEL, BARS, AND FORGINGS, 5.0CR - 1.3MO - 0.50V (0.38 - 0.43C) (H-11), CONSUMABLE ELECTRODE VACUUM MELTED |
| SAE AMS 4677 : 2017 | NICKEL-COPPER ALLOY, CORROSION RESISTANT, BARS AND FORGINGS 66.5NI - 2.9AL - 30CU ANNEALED |
| SAE AMS 6544 : 2013 | STEEL, PLATE, 2.0CR - 10NI - 8.0CO - 1.0MO (0.10 - 0.14C) (HY-180), DOUBLE VACUUM MELTED, SOLUTION HEAT TREATED |
| SAE AMS 2370 : 2016 | QUALITY ASSURANCE SAMPLING AND TESTING, CARBON AND LOW-ALLOY STEEL WROUGHT PRODUCTS AND FORGING STOCK |
| SAE AMS 5906C : 2018 | STEEL, CORROSION-RESISTANT, SHEET AND STRIP, 18CR - 9.0NI (SAE 30302), COLD ROLLED, FULL HARD, 185 KSI (1276 MPA) TENSILE STRENGTH |
| SAE AMS 4408 : 2018 | ALUMINUM ALLOY, PLATE (7140-T7651), 6.6ZN - 1.8CU - 2.0MG - 0.10ZR, SOLUTION HEAT TREATED, STRESS RELIEVED, AND OVERAGED |
| SAE AMS 4326 : 2018 | ALUMINUM ALLOY, 2013, EXTRUDED BAR, ROD, AND PROFILES, 1.0MG - 0.80SI - 1.8CU - 0.20CR (2013- T6511), SOLUTION HEAT TREATED, STRESS-RELIEVED BY STRETCHING, AND AGED |
| SAE AMS 4217 : 2018 | ALUMINUM ALLOY, CASTINGS, 7.0SI - 0.32MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 6557 : 2013 | STEEL, BARS, WIRE, AND FORGINGS, 9V - 5.25CR - 1.3MO (1.80 - 1.95C), POWDER METALLURGY PRODUCT, HOT ISOSTATICALLY PRESSED |
| SAE AMS 2728 : 2012 | HEAT TREATMENT OF WROUGHT COPPER BERYLLIUM ALLOY PARTS |
| SAE AMS 5132L : 2017 | STEEL, BARS, 0.90 - 1.03C |
| SAE AMS 4244 : 2016 | ALUMINUM ALLOY, WELDING WIRE, 4.6CU - 0.35MN - 0.25MG - 0.22TI FOR WELDING A206.0 TYPE ALLOYS |
| SAE AMS 2368 : 2017 | SAMPLING AND TESTING OF WROUGHT TITANIUM RAW MATERIAL EXCEPT FORGINGS AND FORGING STOCK |
| SAE AMS 4485A : 2017 | MAGNESIUM ALLOY, EXTRUSIONS 4.0Y - 2.25ND - 0.5ZR (WE43C - T5) PRECIPITATION HEAT TREATED |
| SAE AMS 3050/2 : 2017 | PERFORMANCE SPECIFICATION ANTI-SEIZE THREAD COMPOUND, HIGH TEMPERATURE - ALUMINUM ONLY |
| 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 |
| SAE AMS 6454 : 2011 | STEEL, SHEET, STRIP, AND PLATE, 1.8NI - 0.80CR - 0.25MO (0.38 - 0.43C) (SAE 4340) VACUUM CONSUMABLE ELECTRODE REMELTED |
| SAE AMS 4174 : 2016 | Aluminum Alloy, Flash Welded Rings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution and Precipitation Heat Treated |
| SAE AMS 4123 : 2011 | ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS AND RODS (7075-T651) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 2371 : 2016 | QUALITY ASSURANCE SAMPLING AND TESTING, CORROSION AND HEAT-RESISTANT STEELS AND ALLOYS, WROUGHT PRODUCTS AND FORGING STOCK |
| SAE AMS 4107 : 2018 | ALUMINUM ALLOY DIE FORGINGS (7050-T74) SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS5554G:2016 | STEEL, CORROSION AND HEAT-RESISTANT, SEAMLESS TUBING, 16.5CR - 4.5NI - 2.9MO - 0.10N, ANNEALED |
| 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 |
| S.R. CWA 16762:2014 | CEN WORKSHOP AGREEMENT - CEN/WS SERES - ICT STANDARDS IN SUPPORT OF AN EREPORTING FRAMEWORK FOR THE ENGINEERING MATERIALS SECTOR |
| SAE AMS 6559 : 2013 | STEEL, BARS, WIRE, AND FORGINGS 9.75V - 5.25CR - 1.3MO (2.40 - 2.55C) POWDER METALLURGY PRODUCT HOT ISOSTATICALLY PRESSED |
| SAE AMS 6371L : 2017 | STEEL, MECHANICAL TUBING, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130) |
| SAE AMS 5918 : 2011 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, BARS, 62CO - 28CR - 6MO, WARM-WORKED |
| SAE AMS 4945 : 2014 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED |
| SAE AMS 6556 : 2013 | STEEL, BARS, WIRE, AND FORGINGS, 8V - 4CR - 4W - 3MO (2.45 - 2.55C), POWDER METALLURGY PRODUCT, HOT ISOSTATICALLY PRESSED |
| SAE AMS 5700G : 2018 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 13.5CR - 13.5NI - 0.35MO - 2.2W, ANNEALED |
| SAE AMS 5714 : 2018 | ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT-RESISTANT, 73NI - 15.5CR - 2.5TI - 0.70AL - 7.0FE, PRECIPITATION-HARDENABLE |
| SAE AMS 5666H : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, EXTRUSIONS, AND RINGS, 62NI - 21.5CR - 9.0MO - 3.65CB (NB), ANNEALED |
| SAE AMS 4443 : 2017 | MAGNESIUM ALLOY, SAND CASTINGS, 4.5ZN - 0.75ZR (ZK51A-T5) PRECIPITATION HEAT TREATED |
| SAE AMS 4340 : 2011 | ALUMINUM ALLOY, EXTRUSIONS, 6.2ZN - 2.3CU - 2.2MG - 0.12ZR (7050-T76511), SOLUTION HEAT TREATED, STRESS RELIEVED, STRAIGHTENED, AND OVERAGED |
| SAE AMS 6931 : 2017 | TITANIUM ALLOY BARS, FORGINGS AND FORGING STOCK, 6.0AL - 4.0V, ANNEALED |
| SAE AMS 7707 : 2018 | IRON, COMMERCIALLY PURE, BAR, SHEET, STRIP, AND PLATE HOT ROLLED, UNANNEALED |
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