F12AA - Nickel Alloy, Corrosion and Heat-Resistant, Bars and Forgings, 57Ni – 20Cr – 10Co – 8.5Mo – 2.1Ti – 1.5Al – 0.005B, Vacuum Induction and Consumable Electrode Melted, Solution Heat Treated, Precipitati

Details Not available for purchase at this time. Document Number: F12AA Project Initiation: 03-07-2012 Project Number: Revision Number: Sponsor Name: Martin R. Christiansen Title Nickel Alloy, Corrosion and Heat-Resistant, Bars and Forgings, 57Ni – 20Cr – 10Co – 8.5Mo – 2.1Ti – 1.5Al – 0.005B, Vacuum Induction and Consumable Electrode Melted, Solution Heat Treated, Precipitati Scope 1.1 Form This specification covers a corrosion and heat-resistant nickel based alloy in the form of bars, forgings and stock for forgings 1.2 Application These products have been used typically for parts requiring high strength up to 1600 °F (871 °C) and oxidation resistance up to 1800 °F (982 °C), but usage is not limited to such applications. Rationale This SAE Aerospace Material Specification is intended to provide technical requirements such as composition, melting practices and heat treatment as well as Quality Assurance provisions for a nickel alloy in the form of bars, forgings and stock for forgings.

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