AMS6522D Steel Plate 2.0Cr - 10Ni - 14Co - 1.0Mo (0.13 - 0.17C) Vacuum Melted, Normalized, and Overaged
Stabilized
02/17/2016
- Features
- Issuing Committee
- Content
- This specification covers a premium aircraft-quality alloy steel in the form of plate.
- Content
- AMS6522D has been stabilized as there are not any users of the document.
- Pages
- 1
- Citation
- SAE International Material Specification, Steel Plate 2.0Cr - 10Ni - 14Co - 1.0Mo (0.13 - 0.17C) Vacuum Melted, Normalized, and Overaged, SAE Standard AMS6522D, Stabilized February 2016, Reaf. Nonc. May 2011, Noncurrent April 2005, Revised July 2003, Issued April 1981, https://doi.org/10.4271/AMS6522D.