SAE AMS4970F
Titanium Alloy, Bars, Wire, and Forgings 7a1 4mo, Solution and Precipitation Heat Treated.
Standard:
AKA:
- AMS4970
- Revision: F
- 1994-04-01
- Historical. Access the latest revision: AMS4970J
- 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 strength up to 900 degrees F (482 degrees C). Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4970J | 2012-09-25 | Latest | |
| AMS4970H | 2008-02-15 | Historical | |
| AMS4970G | 2003-03-14 | Historical | |
| AMS4970F | 1994-04-01 | Historical | |
| AMS4970E | 1984-10-01 | Historical | |
| AMS4970D | 1978-07-15 | Historical | |
| AMS4970C | 1970-05-01 | Historical | |
| AMS4970B | 1969-11-01 | Historical | |
| AMS4970A | 1966-03-15 | Historical | |
| AMS4970 | 1965-09-01 | Historical |
- SAE AMS 4970
- Aerospace
- Nonferrous alloys
- Titanium alloys