AMS6478A Steel, Bars and Forgings 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C) Vacuum Melted, Annealed Heat Treatable to 290 ksi (1999 MPa) Tensile Strength

Revised

10/01/2001

Features
Issuing Committee
Scope
Content
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
Meta TagsDetails
DOI
https://doi.org/10.4271/AMS6478A
Pages
8
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 290 ksi (1999 MPa) Tensile Strength, SAE Standard AMS6478A, Revised October 2001, Issued May 1994, https://doi.org/10.4271/AMS6478A.
Additional Details
Publisher
Published
Oct 1, 2001
Product Code
AMS6478A
Content Type
Material Specification
Status
Revised
Language
English