SAE AMS5670
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings, 72Ni 15.5Cr 0.95Cb 2.5Ti 0.70Al 7.0Fe, 1800°F (982°C) Solution Heat Treated, Precipitation Hardenable.
Standard:
AKA:
- AMS5670
- 1969-05-01
- Historical. Access the latest revision: AMS5670F
- 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 requiring high strength in the range 800 to 1100 degrees F (427 to 593 degrees C), particularly those parts which are formed or welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5670F | 2005-08-29 | Latest | |
| AMS5670E | 1999-01-01 | Historical | |
| AMS5670D | 1996-04-01 | Historical | |
| AMS5670C | 1993-04-01 | Historical | |
| AMS5670B | 1991-10-01 | Historical | |
| AMS5670A | 1981-07-01 | Historical | |
| AMS5670 | 1969-05-01 | Historical |
- SAE AMS 5670
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties