SAE AMS4981C
Titanium Alloy, Bars, Wire, and Forgings, 6.0al 2.0sn 4.0zr 6.0mo, Solution and Precipitation Heat Treated.
Standard:
AKA:
- AMS4981
- Revision: C
- 1994-04-01
- Historical. Access the latest revision: AMS4981F
- Ams G Titanium And Refractory Metals Committee
This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock. Primarily for parts requiring high strength up to 1000 degrees F (538 degrees C). Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking. ARP 982 recommends practices to minimize such conditions.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4981F | 2012-09-14 | Latest | |
| AMS4981E | 2008-01-03 | Historical | |
| AMS4981D | 2003-06-04 | Historical | |
| AMS4981C | 1994-04-01 | Historical | |
| AMS4981B | 1987-07-01 | Historical | |
| AMS4981A | 1981-04-01 | Historical | |
| AMS4981 | 1972-11-15 | Historical |
- SAE AMS 4981
- Aerospace
- Nonferrous alloys
- Titanium alloys