SAE AMS6346A
SAE AMS6346A 2005-SEP-01 Steel Bars 095Cr - 020Mo 028 to 033C SAE 4130 Hardened and Tempered 125 Ks 862 MPa Tensle Strength-UNS G41300
SAE AMS6346A 2005-SEP-01 Steel Bars 095Cr - 020Mo 028 to 033C SAE 4130 Hardened and Tempered 125 Ks 862 MPa Tensle Strength-UNS G41300
Form:
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars.
Application:
These bars have been used typically for parts with sections 1.50 inch (38.1 mm) and under in nominal thickness requiring a minimum tensile strength of 125 ksi (862 MPa), but usage is not limited to such application.