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SAE AMS4242B

SAE AMS4242B 2007-JUL-01 Alumnum Alloy Castngs 47Cu - 060Ag - 035Mn - 025Mg - 025T B2010-T7 Soluton Heat Treated and Overaged

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Form

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

Application

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.

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