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SAE AMS4242

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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Organization: SAE
Publication Date: 1 September 2015
Status: active
Page Count: 10
scope:

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.

Document History

SAE AMS4242
September 1, 2015
Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
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...
July 1, 2007
Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
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...
July 1, 2007
Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
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...
September 1, 1997
(R) Aluminum Alloy Castings, 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
SCOPE: 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,...
July 1, 1986
Aluminum Alloy Castings, Sand Composite 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft Structural Quality
A description is not available for this item.

References

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