SAE AMS4340D
Aluminum Alloy, Extrusions, 6.2zn 2.3cu 2.2mg 0.12zr, Solution Heat Treated, Stress Relieved, Straightened, and Overaged.
Standard:
AKA:
- AMS4340
- Revision: D
- 1998-03-01
- Historical. Access the latest revision: AMS4340E
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
These products have been used typically for structural applications requiring high tensile properties and good exfoliation corrosion resistance, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4340E | 2006-09-14 | Latest | |
| AMS4340D | 1998-03-01 | Historical | |
| AMS4340C | 1989-04-01 | Historical | |
| AMS4340B | 1986-07-01 | Historical | |
| AMS4340A | 1980-07-15 | Historical | |
| AMS4340 | 1977-01-15 | Historical |
- SAE AMS 4340
- Aerospace
- Aluminum alloys
- Aluminum