SAE AMS4167G
Aluminum Alloy, Extrusions, 5.6zn 2.5mg 1.6cu 0.23cr Solution Heat Treated, Stress Relieved By Stretching, and Overaged.
Standard:
AKA:
- AMS4167
- Revision: G
- 1995-07-01
- Historical. Access the latest revision: AMS4167J
- 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 parts subject to excessive warpage during machining 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 |
|---|---|---|---|
| AMS4167J | 2012-01-09 | Latest | |
| AMS4167H | 2005-01-24 | Historical | |
| AMS4167G | 1995-07-01 | Historical | |
| AMS4167F | 1988-04-01 | Historical | |
| AMS4167E | 1979-10-01 | Historical | |
| AMS4167D | 1978-07-01 | Historical | |
| AMS4167C | 1970-05-01 | Historical | |
| AMS4167B | 1968-11-01 | Historical | |
| AMS4167A | 1967-11-01 | Historical | |
| AMS4167 | 1967-04-01 | Historical |
- SAE AMS 4167
- Aerospace
- Aluminum alloys
- Aluminum