SAE AMS6532D
Steel, Bars and Forgings 3.1cr 11.5ni 13.5co 1.2mo (0.21 - 0.25c) Vacuum Melted, Annealed Heat Treatable to 280 Ksi (1931 Mpa) Tensile Strength.
Standard:
AKA:
- AMS6532
- Revision: D
- 2006-02-28
- Historical. Access the latest revision: AMS6532E
- Ams E Carbon And Low Alloy Steels Committee
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS6532E | 2011-06-23 | Latest | |
| AMS6532D | 2006-02-28 | Historical | |
| AMS6532C | 2005-09-22 | Historical | |
| AMS6532B | 2001-10-01 | Historical | |
| AMS6532A | 1995-06-01 | Historical |
- SAE AMS 6532
- Aerospace
- Metallurgy
- Ferrous metals and alloys
- Steel
- Materials properties
- Ferrous metals