SAE AMS6478B
SAE AMS6478B 2005-SEP-01 Steel Bars and Forgngs 31Cr - 115N - 135Co - 12Mo 021 - 025C Vacuum Melted Annealed Heat Treatable to 290 ks 1999 MPa Tensle Strength-UNS K92580 Superseded by SAE AMS6532E
SAE AMS6478B 2005-SEP-01 Steel Bars and Forgngs 31Cr - 115N - 135Co - 12Mo 021 - 025C Vacuum Melted Annealed Heat Treatable to 290 ks 1999 MPa Tensle Strength-UNS K92580 Superseded by SAE AMS6532E
Form: This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
Application: These products have been used typically for parts requiring a combination of high strength, high toughness, and weldability, but usage is not limited to such applications. Product after heat treatment should attain a minimum tensile strength of 290 ksi (1999 MPa) and yield strength of 245 ksi (1689 MPa).