| SAE |
SAE AMS4094 |
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
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| SAE |
SAE AMS4979 |
Titanium Alloy, Bars, Wire, Forgings, and Rings, 6Al - 6V - 2Sn, Solution and Precipitation Heat Treated |
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| SAE |
SAE AMS4972 |
Titanium Alloy Bars, Wire, and Rings, 8Al - 1Mo - 1V, Solution Heat Treated and Stabilized
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| SAE |
SAE AMS4970 |
Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated_x000D_
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| SAE |
SAE AMS5661 |
Nickel-Iron Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings and Stock for Forging or Flash-Welded Rings 42.5Ni - 12.5Cr - 5.8Mo - 2.9Ti - 0.015B - 35Fe (Alloy 901) Consumable Electrode Remelted or Vacuum Induction Melted Solution Heat Treated, Stabilized, and Precipitation Heat Treated
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| SAE |
SAE AMS4965 |
Titanium Alloy, Bars, Wire, Forgings, and Rings, 6.0Al - 4.0V, Solution Heat Treated and Aged |
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| SAE |
SAE AMS4950 |
Titanium Alloy, Bars, Wire, Forgings, and Rings, 6.0Al - 4.0V, Solution Heat Treated and Aged, Modified Strength |
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| BSI |
BS EN 2119 |
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated. Wires for rivets. 2 mm = D = 10 mm. Rm = 960 Mpa |
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| SAE |
SAE AMS4534 |
Copper-Beryllium Alloy, Bars and Rods, 98Cu - 1.9Be, Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (TH04, formerly HT) |
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| SAE |
SAE AMS4975 |
Titanium Alloy, Bars, Wire, and Rings, 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo - 0.08Si, Solution and Precipitation Heat Treated |
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| BSI |
BS EN 4376 |
Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated. Bar and section, De ≤ 200 mm |
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| SAE |
SAE AMS5768 |
Alloy, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Rings and Stock for Forgings, Rings and Heading, 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N - 31Fe, Solution and Precipitation Heat Treated |
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| SAE |
SAE AMS5716 |
Iron-Nickel Alloy, Heat Resistant, Bars, Wire, Forgings, Rings and Stock for Rings and Forgings, 44Fe - 18.5Cr - 35.5Ni - 1.1Si, Solution Heat Treated |
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| SAE |
SAE AMS2241 |
Tolerances, Corrosion- and Heat-Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and Wire |
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| SAE |
SAE MAM2241 |
Tolerances, Metric, Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Bars and Wire |
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| SAE |
SAE AMS5355 |
Steel, Corrosion-Resistant, Investment Castings, 16Cr - 4.1Ni - 0.28Cb - 3.2Cu, Homogenization and Solution Heat Treated or Homogenization, Solution, and Precipitation Heat Treated |
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| SAE |
SAE AMS4120 |
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) |
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| SAE |
SAE AMS4265 |
Aluminum Alloy, Particulate Reinforced Extrusions 6092/Sic/25p - T6p Solution Heat Treated, Quenched, and Precipitation Heat Treated |
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| SAE |
SAE AMS4304 |
Aluminum Alloy, Discontinuously Reinforced Sheet, 2009/SiC/15w (T8P), Solution Heat Treated, Stretched, and Precipitation Heat Treated |
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| ASTM |
D5836 |
Standard Test Method for Determination of 2,4-Toluene Diisocyanate (2,4-TDI) and 2,6-Toluene Diisocyanate (2,6-TDI) in Workplace Atmospheres (1-2 PP Method) |
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| ASTM |
D5932 |
Standard Test Method for Determination of 2,4-Toluene Diisocyanate (2,4-TDI) and 2,6-Toluene Diisocyanate (2,6-TDI) in Air (with 9-(N-Methylaminomethyl) Anthracene Method) (MAMA) in the Workplace |
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| BSI |
BS EN 3510 |
Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Solution treated and precipitation treated. Bars and sections. De = 100 mm |
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| BSI |
BS EN 4318 |
Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De Gëñ 100 mm, Rm GëÑ 960 MPa |
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| BSI |
BS EN 4315 |
Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D Gëñ 100 mm, Rm GëÑ 900 MPa |
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| SAE |
SAE AMS4390 |
Sheet and Plate, Magnesium Alloy, 2.0Th - 0.78Mn (HM21A - T8), Solution Heat Treated, Cold Worked, and Precipitation Heat Treated |
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