SAE AMS4166A
Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution Heat Treated and Overaged.
Standard:
AKA:
- AMS4166
- Revision: A
- 1970-05-01
- Historical. Access the latest revision: AMS4166G
- 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 parts requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4166G | 2012-01-09 | Latest | |
| AMS4166F | 2003-07-28 | Historical | |
| AMS4166E | 1998-03-01 | Historical | |
| AMS4166D | 1991-01-01 | Historical | |
| AMS4166C | 1985-10-01 | Historical | |
| AMS4166B | 1977-01-01 | Historical | |
| AMS4166A | 1970-05-01 | Historical | |
| AMS4166 | 1968-11-01 | Historical |
- SAE AMS 4166
- Aerospace
- Aluminum alloys
- Aluminum