SAE AMS4916H
Titanium Alloy Sheet, Strip, and Plate 8al 1mo 1v Duplex Annealed.
Standard:
AKA:
- AMS4916
- Revision: H
- 2003-10-22
- Historical. Access the latest revision: AMS4916K
- Ams G Titanium And Refractory Metals Committee
This specification covers a titanium alloy in the form of sheet, strip, and plate.
These products have been used typically for parts requiring strength and fracture toughness up to 800 degrees F (427 degrees C), 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; SAE ARP 982 recommends practices to minimize such conditions.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4916K | 2010-04-19 | Latest | |
| AMS4916J | 2006-05-17 | Historical | |
| AMS4916H | 2003-10-22 | Historical | |
| AMS4916G | 2003-04-29 | Historical | |
| AMS4916F | 1994-04-01 | Historical | |
| AMS4916E | 1984-04-01 | Historical | |
| AMS4916D | 1977-01-15 | Historical | |
| AMS4916C | 1976-01-15 | Historical | |
| AMS4916B | 1968-11-01 | Historical | |
| AMS4916A | 1966-09-30 | Historical | |
| AMS4916 | 1966-03-15 | Historical |
- SAE AMS 4916
- Aerospace
- Nonferrous alloys
- Titanium alloys