SAE AMS4343C
Aluminum Alloy, Extrusions, 7.7zn 2.4mg 1.6cu 0.16cr, Solution Heat Treated, Stress Relieved By Stretching, and Overaged.
Standard:
AKA:
- AMS4343
- Revision: C
- 1996-05-01
- Historical. Access the latest revision: AMS4343D
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing.
These extrusions have been used typically for structural parts requiring a combination of high strength, moderate fatigue strength, good stress-corrosion resistance, and good fracture toughness, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4343D | 2004-12-15 | Latest | |
| AMS4343C | 1996-05-01 | Historical | |
| AMS4343B | 1989-01-01 | Historical | |
| AMS4343A | 1987-10-01 | Historical | |
| AMS4343 | 1980-01-15 | Historical |
- SAE AMS 4343
- Aerospace
- Aluminum alloys
- Aluminum