AMS6532B 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
Revised
10/01/2001
- Features
- Issuing Committee
- Content
- This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
- Pages
- 9
- Citation
- SAE International Material Specification, 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, SAE Standard AMS6532B, Revised October 2001, Issued July 1992, https://doi.org/10.4271/AMS6532B.