SAE AMS4342D
Aluminum Alloy, Extrusions 6.2zn 2.3cu 2.2mg 0.12zr (7050-T74511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged.
Standard:
AKA:
- AMS4342
- Revision: D
- 2000-08-01
- Historical. Access the latest revision: AMS4342E
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
These product have been used typically for structural applications requiring a combination of high mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4342E | 2007-08-24 | Latest | |
| AMS4342D | 2000-08-01 | Historical | |
| AMS4342C | 1998-03-01 | Historical | |
| AMS4342B | 1991-10-01 | Historical | |
| AMS4342A | 1986-07-01 | Historical | |
| AMS4342 | 1978-04-15 | Historical |
- SAE AMS 4342
- Aerospace
- Aluminum alloys
- Aluminum