SAE AMS 4242B

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SAE AMS 4242B English Secure PDF Aluminum Alloy, Castings, 4.7Cu 0.60Ag 0.35Mn 0.25Mg 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged ( Reaffirmed: Sep 2012 )

standard published 07/01/2007 by SAE International

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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.