SAE AMS4307A
Aluminum Alloy, Extrusions, 6.4zn 2.4mg 2.2cu 0.12zr, Solution Heat Treated, Stress Relieved By Stretching, Straightened, and Precipitation Heat Treated.
Standard:
AKA:
- AMS4307
- Revision: A
- 1998-03-01
- Historical. Access the latest revision: AMS4307B
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, profiles, and tubing.
These extrustions have been used typically for structural parts requiring a combination of high strength, moderate fatigue strength, and moderate exfoliation corrosion resistance, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4307B | 2005-02-11 | Latest | |
| AMS4307A | 1998-03-01 | Historical | |
| AMS4307 | 1988-10-01 | Historical |
- SAE AMS 4307
- Aerospace
- Aluminum alloys
- Aluminum