SAE AMS5660H
Nickel-Iron Alloy, Corrosion and Heat Resistant, Bars and Forgings 12.5cr 42.5ni 6.0mo 2.7ti 0.015b 34fe, Consumable Electrode Or Vacuum Induction Melted, Solution, Stabilization, and Precipitation Heat Treated.
Standard:
AKA:
- AMS5660
- Revision: H
- 1995-12-01
- Historical. Access the latest revision: AMS5660K
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel-iron alloy in the form of bars, forgings, and forging stock.
These products have been used typically for parts, such as turbine rotors, shafts, and blades, requiring high strength up to 1400 degrees F (760 degrees C) and oxidation resistance up to 1600 degrees F (871 degrees C), but usate is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5660K | 2008-01-03 | Latest | |
| AMS5660J | 2002-08-21 | Historical | |
| AMS5660H | 1995-12-01 | Historical | |
| AMS5660G | 1988-04-01 | Historical | |
| AMS5660F | 1981-07-01 | Historical | |
| AMS5660E | 1971-05-01 | Historical | |
| AMS5660D | 1970-05-01 | Historical | |
| AMS5660C | 1967-11-01 | Historical | |
| AMS5660B | 1966-03-01 | Historical | |
| AMS5660A | 1960-01-01 | Historical | |
| AMS5660 | 1959-06-01 | Historical |
- SAE AMS 5660
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties