SAE AMS4972D
Titanium Alloy, Bars, Wire, and Rings, 8a1 1mo 1v, Solution Heat Treated and Stabilized.
Standard:
AKA:
- AMS4972
- Revision: D
- 1994-04-01
- Historical. Access the latest revision: AMS4972G
- Ams G Titanium And Refractory Metals Committee
This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock or flash welded rings or heading. Primarily for parts requiring strength up to 800 degrees F (427 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 |
|---|---|---|---|
| AMS4972G | 2011-09-13 | Latest | |
| AMS4972F | 2007-10-16 | Historical | |
| AMS4972E | 2003-01-07 | Historical | |
| AMS4972D | 1994-04-01 | Historical | |
| AMS4972C | 1985-01-01 | Historical | |
| AMS4972B | 1979-01-15 | Historical | |
| AMS4972A | 1970-05-01 | Historical | |
| AMS4972 | 1966-03-15 | Historical |
- SAE AMS 4972
- Aerospace
- Nonferrous alloys
- Titanium alloys