SAE AMS4225C
Aluminum Alloy, Heat Resistant, Castings 5.0cu 1.5ni 0.25mn 0.25sb 0.25co 0.20ti 0.20zr, Solution Heat Treated and Stabilized.
Standard:
AKA:
- AMS4225
- Revision: C
- 1996-07-01
- Historical. Access the latest revision: AMS4225D
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of castings.
These castings have been used typically for components requiring moderate strength and good stability up to 600 degrees F (316 degrees C) with resistance to stress-corrosion cracking, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4225D | 2007-06-27 | Latest | |
| AMS4225C | 1996-07-01 | Historical | |
| AMS4225B | 1995-05-01 | Historical | |
| AMS4225A | 1984-04-01 | Historical | |
| AMS4225 | 1968-11-01 | Historical |
- SAE AMS 4225
- Aerospace
- Aluminum alloys
- Aluminum