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 be used at temperatures up to 650°C (1200°F) which is critical rotating applications. WASPALOYContinue reading “DMD 0246-22”

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 temperatures up to 1300ºF and oxidation resistance to 1800ºF. Alloy 718 is used in applicationsContinue reading “MTS 1424-3”

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 up to 1300ºF and oxidation resistance to 1800ºF. Alloy 718 is used in applications thatContinue reading “MTS 1424-1”

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 1300ºF and oxidation resistance to 1800ºF. Alloy 718 is used in applications that require highContinue reading “BMS7-340”

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 your project callout specification DMS 2209?   Boeing holds its subcontractors to the same standards byContinue reading “DMS 2209”

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 nationale d’études et de construction de moteurs d’aviation or Snecma Moteurs) is a French aerospace engine manufacturerContinue reading “HMDM0022”

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 transverse strength and toughness such as engine parts, aircraft components, nuclear reactor components etc.  Continue reading “ASNA 3294”