SAE AMS4242A
Aluminum Alloy, Castings, 4.7cu 0.60ag 0.35mn 0.25mg 0.25ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft.
Standard:
AKA:
- AMS4242
- Revision: A
- 1997-09-01
- Historical. Access the latest revision: AMS4242B
- Ams D Nonferrous Alloys Committee
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.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4242B | 2007-07-13 | Latest | |
| AMS4242A | 1997-09-01 | Historical | |
| AMS4242 | 1986-07-01 | Historical |
- SAE AMS 4242
- Aerospace
- Aluminum alloys
- Aluminum