SAE AMS5711C
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 65ni 15.8cr 15.2mo 0.30al 0.05la, Solution Heat Treated.
Standard:
AKA:
- AMS5711
- Revision: C
- 1996-04-01
- Historical. Access the latest revision: AMS5711D
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
These products have been used typically for parts, such as turbine rotors and seals, flanges, and fasteners requiring relatively high strength up to 1800 degrees F (982 degrees C) and oxidation resistance up to 2000 degrees F (1093 degrees C), but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5711D | 2002-11-21 | Latest | |
| AMS5711C | 1996-04-01 | Historical | |
| AMS5711B | 1990-01-01 | Historical | |
| AMS5711A | 1983-07-01 | Historical | |
| AMS5711 | 1973-12-01 | Historical |
- SAE AMS 5711
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties