SAE AMS4911H
Titanium Alloy, Sheet, Strip, and Plate, 6a1 4v, Annealed.
Standard:
AKA:
- AMS4911
- Revision: H
- 1995-07-01
- Historical. Access the latest revision: AMS4911M
- Ams G Titanium And Refractory Metals Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate procured in inch/pound units.
MAM 4911 is the metric version of this AMS.
These products have been used typically for parts requiring strength up to 750 degrees F, but usage is not limited to such applications.
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 |
|---|---|---|---|
| AMS4911M | 2012-01-06 | Latest | |
| AMS4911L | 2007-06-27 | Historical | |
| AMS4911K | 2007-02-27 | Historical | |
| AMS4911J | 2003-03-14 | Historical | |
| AMS4911H | 1995-07-01 | Historical | |
| AMS4911G | 1994-03-01 | Historical | |
| AMS4911F | 1988-04-01 | Historical | |
| AMS4911E | 1984-10-01 | Historical | |
| AMS4911D | 1977-01-15 | Historical | |
| AMS4911C | 1973-12-01 | Historical | |
| AMS4911B | 1968-05-01 | Historical | |
| AMS4911A | 1963-07-15 | Historical | |
| AMS4911 | 1957-07-01 | Historical |
- SAE AMS 4911
- Aerospace
- Nonferrous alloys
- Titanium alloys