SAE AMS5671A
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings and Rings 72Ni 15.5Cr 0.95Cb 2.5Ti 0.70Al 7.0Fe, Consumable Electrode or Vacuum Induction Melted 1800°F (982°C) Solution Heat Treated, Precipitation Hardenable.
Standard:
AKA:
- AMS5671
- Revision: A
- 1968-05-01
- Historical. Access the latest revision: AMS5671G
- 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 and flash welded rings.
These products have been used typically for parts requiring high strength at temperatures in the range 800 1100 degrees F (427 to 593 degrees C), particularly those which are formed or welded, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5671G | 2003-01-23 | Latest | |
| AMS5671F | 1996-09-01 | Historical | |
| AMS5671E | 1989-07-01 | Historical | |
| AMS5671D | 1979-10-01 | Historical | |
| AMS5671C | 1978-01-01 | Historical | |
| AMS5671B | 1969-11-01 | Historical | |
| AMS5671A | 1968-05-01 | Historical | |
| AMS5671 | 1965-09-01 | Historical |
- SAE AMS 5671
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties