SAE AMS4089D
Aluminum Alloy, Plate 1.6Cu - 2.2Mg - 0.22Cr - 5.7Zn (7475-T7651) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated.
Standard:
AKA:
- AMS4089
- Revision: D
- 2008-05-01
- 2003-10-23
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of plate.
This plate has been used typically for structural applications requiring material with high strength and resistance to exfoliation-corrosion, moderate fatigue strength, and high fracture-toughness, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4089D | 2003-10-23 | Latest | |
| AMS4089C | 1998-10-01 | Historical | |
| AMS4089B | 1992-04-01 | Historical | |
| AMS4089A | 1978-10-01 | Historical | |
| AMS4089 | 1976-07-01 | Historical |
- SAE AMS 4089
- Aerospace
- Aluminum alloys
- Aluminum