SAE AMS4078F
Aluminum Alloy Plate (7075-T7351) Solution Heat Treated, Stress Relieved, and Overaged.
Standard:
AKA:
- AMS4078
- Revision: F
- 2000-02-01
- Historical. Access the latest revision: AMS4078J
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of plate.
This plate has been used typically for machined parts subject to excessive warpage during machining due to residual stresses and for parts requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4078J | 2011-10-21 | Latest | |
| AMS4078H | 2010-12-29 | Historical | |
| AMS4078G | 2007-02-27 | Historical | |
| AMS4078F | 2000-02-01 | Historical | |
| AMS4078E | 1992-07-01 | Historical | |
| AMS4078D | 1991-10-01 | Historical | |
| AMS4078C | 1984-04-01 | Historical | |
| AMS4078B | 1974-12-01 | Historical | |
| AMS4078A | 1967-11-01 | Historical | |
| AMS4078 | 1967-04-01 | Historical |
- SAE AMS 4078
- Aerospace
- Aluminum alloys
- Aluminum