SAE AMS4249
Aluminum Alloy, Castings 7.0si 0.58mg 0.15ti 0.06be Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing).
Standard:
AKA:
- AMS4249
- 1992-07-01
- Historical. Access the latest revision: AMS4249A
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of castings. These castings have been used typically for durability and damage tolerance structural aircraft components requiring fatigue resistance and fracture toughness, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4249A | 2005-03-03 | Latest | |
| AMS4249 | 1992-07-01 | Historical |
- SAE AMS 4249
- Aerospace
- Aluminum alloys
- Aluminum
- Tests and Testing