SAE AMS4242 Revision B

SAE AMS4242 – Revision B – Aluminum Alloy, Castings, 4.7Cu – 0.60Ag – 0.35Mn – 0.25Mg – 0.25Ti (B201.0-T7), Solution Heat Treated and Overaged

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.

Product Details

Published:

07/13/2007

File Size:

1 file , 1 MB

Note:

This product is unavailable in Ukraine, Russia, Belarus