SAE AMS4252A
Aluminum Alloy, Plate 6.4zn 2.4mg 2.2cu 0.12zr, Solution Heat Treated, Stress Relieved, and Overaged.
Standard:
AKA:
- AMS4252
- Revision: A
- 1995-03-01
- Historical. Access the latest revision: AMS4252B
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of plate.
This plate has been used typically for structural applications requiring a combination of high tensile strength and compressive properties and good exfoliation corrosion resistance, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4252B | 2005-03-03 | Latest | |
| AMS4252A | 1995-03-01 | Historical | |
| AMS4252 | 1989-10-01 | Historical |
- SAE AMS 4252
- Aerospace
- Aluminum alloys
- Aluminum