D11AE - Copper-Nickel-Tin Alloy, Tubes, Solution Annealed, Cold Finished and Spinodal Hardened (TXTS)

Details Not available for purchase at this time. Document Number: D11AE Project Initiation: 04-19-2011 Project Number: Revision Number: Sponsor Name: W Raymond Cribb Title Copper-Nickel-Tin Alloy, Tubes, Solution Annealed, Cold Finished and Spinodal Hardened (TXTS) Scope This new specification is for high strength cold worked tube of Cu-15Ni-8Sn (C72900) alloy after spinodal hardening for use in highly loaded bushing/bearing components. Outside diameter includes1.625 to 2.500 inch with wall thickness less than 20% of the outside diameter. Rationale This SAE Aerospace Material Specification is intended to provide technical requirements such as composition, casting practices and heat treatment as well as Quality Assurance provisions drawn C72900 alloy.

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