SAE AMS4121G
Aluminum Alloy Bars, Rods, and Wire, Rolled Or Cold Finished, 4.5cu 0.85si 0.80mn 0.50mg (2014-T6) Solution and Precipitation Heat Treated.
Standard:
AKA:
- AMS4121
- Revision: G
- 1998-01-01
- Historical. Access the latest revision: AMS4121H
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of bars, rods, and wire. Primarily for parts requiring high strength where limited formability is acceptable. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP 823 recommends practices to minimize such conditions.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4121H | 2007-11-16 | Latest | |
| AMS4121G | 1998-01-01 | Historical | |
| AMS4121F | 1992-04-01 | Historical | |
| AMS4121E | 1978-07-01 | Historical | |
| AMS4121D | 1967-11-01 | Historical | |
| AMS4121C | 1964-01-01 | Historical | |
| AMS4121B | 1958-01-01 | Historical | |
| AMS4121A | 1951-12-01 | Historical | |
| AMS4121 | 1946-11-01 | Historical |
- SAE AMS 4121
- Aerospace
- Aluminum alloys
- Aluminum