SAE AMS5661D
Nickel-Iron Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 42.5ni 12.5cr 5.8mo 2.9ti 0.015b 35fe Consumable Electrode Or Vacuum Induction Melted Solution, Stabilization, and Precipitation Heat Treated.
Standard:
AKA:
- AMS5661
- Revision: D
- 1989-04-01
- Historical. Access the latest revision: AMS5661F
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel-iron alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
These products have been used typically for parts, such as turbine discs, shafts, and blades, requiring high strength than AMS 5660 up to 1400 °F (760 °C) and oxidation resistance up to 1600 °F (871 °C), but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5661F | 2005-08-29 | Latest | |
| AMS5661E | 1995-12-01 | Historical | |
| AMS5661D | 1989-04-01 | Historical | |
| AMS5661C | 1983-10-01 | Historical | |
| AMS5661B | 1972-11-01 | Historical | |
| AMS5661A | 1966-03-01 | Historical | |
| AMS5661 | 1964-01-01 | Historical |
- SAE AMS 5661
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties