Tag: Bars

DMD 0246-22

REQUEST QUOTE DMD 0246-22 is a Snecma / Safran specification for Waspaloy Bars and Forgings WASPALOY is a nickel based age hardenable alloy that possesses high temperature strength while still having a good corrosion resistance, especially to oxidation. WASPALOY can…

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B50A809

REQUEST QUOTE B50A809 is a GE Aviation Specification for Nickel 718 Bars and Forgings Nickel / Inconel 718 is used in applications that require high strength such as parts for jet engines and high speed airframe parts such as wheels,…

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B50TF15

REQUEST QUOTE B50TF15 is a GE Aviation Specification for Nickel 718 Bars and Forgings B50TF15 has designations for different finishes of 718: B50TF15 A B50TF15 D B50TF15 E Nickel / Inconel 718 is used in applications that require high strength…

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MTS 1424-3

REQUEST QUOTE MTS 1424-3 is a MTU Aero Engines specification for Nickel 718 / Inconel 718 Bars and Forgings   Alloy 718 (UNS N07718) is an austenitic nickel-based superalloy. Alloy 718 exhibits excellent high yield tensile and creep-rupture properties at…

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MTS 1424-1

REQUEST QUOTE MTS 1424-1 is a MTU Aero Engines specification for Nickel 718 / Inconel 718 Bars and Forgings Alloy 718 (UNS N07718) is an austenitic nickel-based superalloy. Alloy 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures…

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BMS7-340

REQUEST QUOTE BMS 7-340 is a NICKEL 718 Boeing Material Specification for “NICKEL-BASE ALLOY, NICKEL ALLOY 718 (UNS N07718)” Nickel 718 is an austenitic nickel-based superalloy. Alloy 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to…

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DMS 2209

REQUEST QUOTE DMS 2209 is a BOEING specification for NICKEL 718 for “NICKEL BASE ALLOY BAR & WIRE, STRAIN HARDENED, CORROSION & HEAT RESISTANT, UNS N07718” DMS specifications originate from Boeing’s Long Beach facility under D1-4426 Approved Process Lists.   Why does…

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HMDM0022

REQUEST QUOTE 15-5 PH Stainless Steel per Aircelle / Safran HMDM0022 Round Bar and Forgings 15-5 PH Stainless Steel is a precipitation hardening alloy. 15-5 PH exhibits high strength and hardness with moderate corrosion resistance (CRES).   Safran Aircraft Engines (previously Snecma, Société…

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B50TF31-A

REQUEST QUOTE B50TF31-A is a GE Aviation Specification for Hastelloy X Bars and Forgings under AMS 5754 HASTELLOY X per B50TF31-A is a wrought nickel base alloy with excellent high temperature strength and oxidation resistance. All of the product forms…

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ASNA 3294

REQUEST QUOTE 15-5 PH per Airbus specification ASNA 3294 15-5 PH Stainless Steel is a precipitation hardening alloy. 15-5 PH exhibits high strength and hardness with moderate corrosion resistance (CRES). 15-5 PH Stainless Steel is used in applications that require high…

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