SAE AMS5596J
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, Foil, and Plate 52.5Ni 19Cr 3.0Mo 5.1Cb 0.90Ti 0.50Al 18Fe Consumable Electrode or Vacuum Induction Melted, 1775°F (968°C) Solution Heat Treated.
Standard:
AKA:
- AMS5596
- Revision: J
- 1999-07-01
- Historical. Access the latest revision: AMS5596K
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, foil, and plate.
These products have been used typically for parts requiring resistance to creep and stress-rupture up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), particularly those parts which are formed or welded and then heat treated to develop desired properties, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5596K | 2007-05-15 | Latest | |
| AMS5596J | 1999-07-01 | Historical | |
| AMS5596H | 1996-08-01 | Historical | |
| AMS5596G | 1987-04-01 | Historical | |
| AMS5596F | 1987-01-01 | Historical | |
| AMS5596E | 1984-07-01 | Historical | |
| AMS5596D | 1981-04-01 | Historical | |
| AMS5596C | 1968-11-01 | Historical | |
| AMS5596B | 1967-11-01 | Historical | |
| AMS5596A | 1964-06-01 | Historical | |
| AMS5596 | 1964-01-01 | Historical |
- SAE AMS 5596
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties