ABS5441

REQUEST QUOTE ABS5441 is an Airbus Specification for Nickel 718 Plate similar to AMS 5596   Nickel 718 (UNS N07718) is an austenitic nickel-based superalloy. Nickel / Inconel 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to 1300ºF and oxidation resistance to 1800ºF. Nickel 718 is used in applications that requireContinue reading “ABS5441”

ABS5440

REQUEST QUOTE ABS5440 is an Airbus Specification for Nickel 718 Plate similar to AMS 5596 Nickel 718 (UNS N07718) is an austenitic nickel-based superalloy. Nickel / Inconel 718 exhibits excellent high yield tensile and creep-rupture properties at temperatures up to 1300ºF and oxidation resistance to 1800ºF. Nickel 718 is used in applications that require highContinue reading “ABS5440”

IPS 01-04-003-02

REQUEST QUOTE 15-5 PH Stainless Steel per Airbus Specification IPS 01-04-003-02 15-5 PH per AMS 5659 stainless steel is a martensitic precipitation-hardening stainless steel with approximately 15% Chromium and 5% Nickel. It has high strength, high hardness, and excellent corrosion resistance. Strength can be further increased by a single low temperature heat treatment. Airbus SpecificationsContinue reading “IPS 01-04-003-02”

ABS 5455

15-5 PH per Airbus specification ABS 5455 REQUEST QUOTE 15-5 PH Stainless Steel per ABS 5455 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 reactorContinue reading “ABS 5455”

ABS 5750

REQUEST QUOTE 15-5 PH per Airbus specification ABS 5750 15-5 PH Stainless Steel per ABS 5750 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 reactorContinue reading “ABS 5750”

ASNA 6116

REQUEST QUOTE 15-5 PH per Airbus specification ASNA 6116 15-5 PH Stainless Steel per ASNA 6116 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 reactorContinue reading “ASNA 6116”

ASNA 3297

REQUEST QUOTE 15-5 PH per Airbus specification ASNA 3297 15-5 PH Stainless Steel per Airbus ASNA 3297 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,Continue reading “ASNA 3297”

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”

IPS 01-04-004

REQUEST QUOTE PH 13-8 Mo per Airbus specification  Ph 13-8 Mo is a martensitic precipitation-hardening stainless steel that has excellent strength, high hardness, superior toughness, and good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content, and vacuum melting. The alloy is produced by vacuum induction melting (VIM)Continue reading “IPS 01-04-004”