Browse Standards AMS4242A
Historical Revised 1997-09-01

Aluminum Alloy, Castings, 4.7cu 0.60ag 0.35mn 0.25mg 0.25ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft AMS4242A

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, 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.

AMS4242C
2015-09-01
Latest
Revised
AMS4242B
2012-09-27
Historical
Reaffirmed
AMS4242A
1997-09-01
Historical
Revised
AMS4242
1986-07-01
Historical
Issued

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