TDS PDF

Steel, Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Aircraft Quality, Normalized or Otherwise Heat Treated. Original standard SAE AMS6345F-2024 in PDF full version. Additional info + preview on request

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Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Aircraft Quality Hardened and Tempered, 125 ksi (862 MPa) Tensile Strength. Original standard SAE AMS6346D-2023 in PDF full version. Additional info + preview on request

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Steel, Bars Aircraft Quality 0.95Cr - 0.20Mo (0.28 to 0.33C) (4130) Normalized. Original standard SAE AMS6348F-2023 in PDF full version. Additional info + preview on request

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Steel Bars 0.95Cr - 0.20Mo (0.38 to 0.43C) (SAE 4140) Normalized. Original standard SAE AMS6349F-2024 in PDF full version. Additional info + preview on request

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Steel Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Aircraft Quality. Original standard SAE AMS6350R-2024 in PDF full version. Additional info + preview on request

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Steel, Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Aircraft Quality, Spheroidized. Original standard SAE AMS6351M-2024 in PDF full version. Additional info + preview on request

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