Non-Corrosion Resisting Steel DTD 5082

Technical Data Sheet   Chemical Composition Limits Weight% C Si Mn P+S max Cr Mo Ni DTD 5082 0.18-0.26 0.10-0.35 0.40-0.80 P 0.020 S 0.015 0.80-1.20 0.15-0.25 0.50 max Other Chemically similar Specifications Weight% C Si Mn P+S max Cr Mo Ni AFNOR 25C04 0.22-0.28 0.10-0.40 0.60-0.90 P 0.035 S 0.035 0.85-1.15 0.15-0.30 – WS 1.7218 0.22-0.29 0.15-0.40 0.50-0.80 P …

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Aircraft Stainless Steel BS T72 seamless tube

Technical Data Sheet BS T72 is the British aerospace standard for seamless tube in stainless steel 347 with the addition of copper. It is often dual certified to BS T66 and offers good corrosion resistance and good weldability. T72 is designed for use in hydraulic applications. Chemical Composition Limits Weight% C Cu Si Mn Cr Ni Nb P+S max T72 …

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Carbon Manganese Steel Tube T64

Technical Data Sheet   Chemical Composition Limits Weight% C Si Mn Cr Ni Mo T64 Tube 0.17-0.25 0.10-0.35 1.30-1.70 0.25 0.40 max 0.10 Typical Mechanical Properties Grade Treatment Tensile Strength Rm , N/mm² Yield Strength, N/mm² Hardness HB Ruling Section T64Tube Cold Drawn + Tempered 550-750 460 152-217 3/16" OD to 7/16" OD Availability Alloy T64 Tube. For all stock …

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Chrome Molybdenum Steel Tube T60

Technical Data Sheet   Chemical Composition Limits Weight% C Si Mn Cr Ni Mo P + S max 3 T60 Tube 0.22-0.29 0.15-0.35 0.50-0.80 0.90-1.20 0.30 max 0.15-0.25 P 0.020 S 0.015 Typical Mechanical Properties Grade Treatment Tensile Strength Rm , N/mm² Yield Strength, N/mm² Elongation (%) Hardness HB Ruling Section 3 T60 Tube Hardened and Tempered 1150-1350 1050 6 …

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Aircraft Carbon Steel BS T45/ 4T45 Tube

Technical Data Sheet BS T45 is a carbon-manganese steel tube supplied in the hardened and tempered condition. It finds many different applications in both the motorsport and aerospace industries due to its high strength to weight ration. T45 is also weldable, but unlike other chome-moly tube grades does not require heat treating after welding. Chemical Composition Limits Weight% C Si …

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Aircraft Steel BS S535

Technical Data Sheet BS S535 is an alloy steel, similar to U.S. specification 4130 (AMS 6350). It is supplied in sheet form in the softened condition, usually dual certified to BS S534 for subsequent heat treatment, depending on the properties required. Heat treatment is as follows: S534 Harden 870°C + Oil quench / Temper 540°C (2hrs) + air cool S535 …

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4130 (AMS 6345/ AMS 6346 / AMS 6350)- Chrome-Moly Aircraft Steel

Technical Data Sheet Alloy 4130 (AISI 4130) is a chromium molybdenum alloy steel being a widely used Aircraft Steel due to its weldability, ease of fabrication and mild hardenability. The hardenability and weldability of Alloy 4130 are considered equivalent to 8630 (MIL-S-6250) . Alloy 4130 is also vacuum degassed to meet the magnetic particle inspection standards of AMS 2301. Applications of 4130 …

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Alloy Steel S534

Technical Data Sheet BS S534 is an alloy steel, similar to U.S. specification 4130 (AMS 6350). It is supplied in sheet form in the softened condition, usually dual certified to BS S535 for subsequent heat treatment, depending on the properties required. Heat treatment is as follows: S534 Harden 870°C + Oil quench / Temper 540°C (2hrs) + air cool S535 …

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