SAE AMS5771
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings and Rings, 74Ni - 7.0Cr - 16.5Mo, Solution Heat Treated.
Standard:
AKA:
- AMS5771
- 1971-05-01
- Historical. Access the latest revision: AMS5771F
- 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 or flash welded rings.These products have been used typically for parts, such as turbine air-sealing components, requiring moderate strength up to 1400 °F (760 °C) and oxidation resistance up to 1600 °F (871 °C), particularly where a low coefficient of expansion is desirable, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5771F | 2009-04-14 | Latest | |
| AMS5771E | 2004-01-12 | Historical | |
| AMS5771D | 1996-04-01 | Historical | |
| AMS5771C | 1989-01-01 | Historical | |
| AMS5771B | 1982-01-01 | Historical | |
| AMS5771A | 1979-07-01 | Historical | |
| AMS5771 | 1971-05-01 | Historical |
- SAE AMS 5771
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties