SAE AMS4915J
Titanium Alloy Sheet, Strip, and Plate 8al 1v 1mo Single Annealed.
Standard:
AKA:
- AMS4915
- Revision: J
- 2003-08-14
- Historical. Access the latest revision: AMS4915L
- 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 up to 800 degrees F (427 degrees C) where fracture toughness is not critical.
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 |
|---|---|---|---|
| AMS4915L | 2013-02-26 | Latest | |
| AMS4915K | 2008-12-19 | Historical | |
| AMS4915J | 2003-08-14 | Historical | |
| AMS4915H | 2003-06-16 | Historical | |
| AMS4915G | 1994-04-01 | Historical | |
| AMS4915F | 1984-04-01 | Historical | |
| AMS4915E | 1977-07-15 | Historical | |
| AMS4915D | 1977-01-15 | Historical | |
| AMS4915C | 1976-01-15 | Historical | |
| AMS4915B | 1968-11-01 | Historical | |
| AMS4915A | 1966-09-30 | Historical | |
| AMS4915 | 1966-03-15 | Historical |
- SAE AMS 4915
- Aerospace
- Nonferrous alloys
- Titanium alloys