SAE AMS4050B
Aluminum Alloy, Plate 6.2zn 2.3cu 2.2mg 0.12zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged.
Standard:
AKA:
- AMS4050
- Revision: B
- 1984-04-01
- Historical. Access the latest revision: AMS4050H
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of plate.
This plate has been used typically for parts requiring a high level of mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4050H | 2003-12-12 | Latest | |
| AMS4050G | 2000-06-01 | Historical | |
| AMS4050F | 1998-11-01 | Historical | |
| AMS4050E | 1992-07-01 | Historical | |
| AMS4050D | 1991-10-01 | Historical | |
| AMS4050C | 1984-10-01 | Historical | |
| AMS4050B | 1984-04-01 | Historical | |
| AMS4050A | 1977-07-01 | Historical | |
| AMS4050 | 1974-12-01 | Historical |
- SAE AMS 4050
- Aerospace
- Aluminum alloys
- Aluminum