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About This Item

 

Full Description

This specification covers an aluminum alloy in the form of castings.

These castings have been used typically for aircraft components requiring high strength and reliability, both at room and elevated temperatures, but usage is not limited to such applications.

Alloy B201.0, the alloy designated in this specification, has restricted composition within the limits of alloy A201.0.
 

Document History

  1. SAE AMS4242C


    Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged

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  2. SAE AMS4242B

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    Aluminum Alloy, Castings, 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7), Solution Heat Treated and Overaged

    • Historical Version