SAE AMS5708F
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 58Ni 19.5Cr 13.5Co 4.3Mo 3.0Ti 1.4Al Consumable Electrode or Vacuum Induction Melted 1975°F (1079°C) Solution Heat Treated.
Standard:
AKA:
- AMS5708
- Revision: F
- 1990-04-01
- Historical. Access the latest revision: AMS5708K
- 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 bolts and turbine blades, requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1750 degrees F (954 degrees C), but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5708K | 2008-03-27 | Latest | |
| AMS5708J | 2006-09-08 | Historical | |
| AMS5708H | 2002-11-21 | Historical | |
| AMS5708G | 1995-12-01 | Historical | |
| AMS5708F | 1990-04-01 | Historical | |
| AMS5708E | 1981-10-01 | Historical | |
| AMS5708D | 1981-01-15 | Historical | |
| AMS5708C | 1973-12-01 | Historical | |
| AMS5708B | 1970-11-01 | Historical | |
| AMS5708A | 1970-05-01 | Historical | |
| AMS5708 | 1963-07-15 | Historical |
- SAE AMS 5708
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties