SAE AMS5605C
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 41.5Ni 16Cr 37Fe 2.9Cb 1.8Ti Consumable Electrode or Vacuum Induction Melted, 1800°F (982°C) Solution Heat Treated.
Standard:
AKA:
- AMS5605
- Revision: C
- 1992-10-01
- Historical. Access the latest revision: AMS5605F
- Ams F Corrosion Heat Resistant Alloys Committee
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate 1.00 inch (25.4 mm) and under in nominal thickness.
These products have been used typically for parts requiring good machinability and high strength at room and cryogenic temperatures and for short-time use up to 1000 degrees F (538 degrees C), particularly for those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS5605F | 2013-08-12 | Latest | |
| AMS5605E | 2006-09-22 | Historical | |
| AMS5605D | 2000-10-01 | Historical | |
| AMS5605C | 1992-10-01 | Historical | |
| AMS5605B | 1991-10-01 | Historical | |
| AMS5605A | 1979-07-01 | Historical | |
| AMS5605 | 1971-11-01 | Historical |
- SAE AMS 5605
- Aerospace
- Metallurgy
- Metals
- Nickel
- Materials properties