Stainless Steel 347 (AMS 5512 / AMS 5646)

Technical Data Sheet Alloy 347 is a chromium nickel stainless steel which has been modified by the addition of columbium and tantalum. The main advantage of this is an excellent resistance to intergranular corrosion which is common to other austenitic stainless steels following exposure to temperatures of 800° to 1500°F. Type 347 has about the same general corrosion resistance as …

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Aircraft Stainless Steel BS S527 (AMS 5512)

Technical Data Sheet BS S527 is the British aerospace standard for stainless steel 347, and is often supplied dual-certified to the U.S. aerospace specification AMS 5512. It is supplied in the annealed condition to allow good cold workability and is suitable for low strength components requiring good corrosion resistance and weldability. Chemical Composition Limits Weight% C Si Mn P + …

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Aircraft Stainless Steel BS S526 (AMS 5689)

Technical Data Sheet BS S526 is the British aerospace standard for stainless steel 321, and is often supplied dual-certified to the U.S. aerospace specification AMS 5510. It is supplied in the annealed condition to allow good cold workability and is suitable for low strength components requiring good corrosion resistance and weldability. Chemical Composition Limits Weight% C Si Mn Cr Mo …

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Stainless Steel 321 (AMS 5510 / AMS 5645)

Technical Data Sheet Type 321 is a chromium-nickel stainless steel and with the addition of titanium, type 321 is resistant to intergranular corrosion. Type 321\’s general corrosion is less than Type 302.  Type 321 is used where resistance to intergranular corrosion is required and where the parts are subjected to sustained heating or cooling within the range of 800 to 1500ºF. …

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Carbon Steel S511

Technical Data Sheet BS S511 is a heat treatable carbon steel that is mainly used in low strength applications where significant drawing is required during the manufacture process. Chemical Composition Limits Weight% C Si Mn P + S max Cr Mo Ni S511 0.1 max 0.2 max 0.5 max P 0.04 S 0.04 0.15 max 0.1 max 0.3 max Typical …

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Aircraft Stainless Steel Jethete M152 (BS S151/ S159)

Technical Data Sheet Jethete M152 is a creep and corrosion resistant, hardened and tempered steel with a usual upper temperature limit of 560°C. It combines very good toughness and creep rupture properties making it an excellent alloy for use in highly stressed turbine blades, discs, screws, bolts and rings. Jethete M152 is supplied by Aircraft Materials in both bar form, …

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Non-Corrosion Resisting Steel S157 / 3S107

Technical Data Sheet   Chemical Composition Limits Weight% C Si Mn P+S max Cr Mo Ni S157 0.12-0.17 0.15-0.40 0.30-0.60 P 0.025 S 0.020 0.80-1.10 0.20-0.30 3.00-3.50 Chemically similar British Specifications BS.970 Pt3 Weight% C Si Mn P+S max Cr Mo Ni 832H13 832M13 0.10-0.16 0.10-0.35 0.35-0.60 P 0.040 S 0.050 0.70-1.00 0.10-0.25 3.00-3.75 EN36A 0.12-0.18 0.10-0.35 0.30-0.60 0.050 0.60-1.10 …

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