SAE AMS5754K
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 47.5ni 22cr 1.5co 9mo 0.60w 18.5fe, Solution Heat Treated.
Standard:
AKA:
- AMS5754
- Revision: K
- 1995-12-01
- Historical. Access the latest revision: AMS5754M
- 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, shafts, flanges, blades, and bolts, requiring oxidation resistance up to 2200 degrees F (1204 degrees C) and relatively high strength above 1500 degrees F (816 degrees C), but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5754M | 2007-08-24 | Latest | |
| AMS5754L | 2002-08-21 | Historical | |
| AMS5754K | 1995-12-01 | Historical | |
| AMS5754J | 1990-01-01 | Historical | |
| AMS5754H | 1984-01-01 | Historical | |
| AMS5754G | 1977-07-01 | Historical | |
| AMS5754F | 1968-11-01 | Historical | |
| AMS5754E | 1965-09-01 | Historical | |
| AMS5754D | 1961-07-01 | Historical | |
| AMS5754C | 1960-11-01 | Historical | |
| AMS5754B | 1960-06-01 | Historical | |
| AMS5754A | 1960-01-01 | Historical | |
| AMS5754 | 1954-05-01 | Historical |
- SAE AMS 5754
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties