SAE AMS6346A-2009
Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength

Standard No.

SAE AMS6346A-2009

Release Date

2009

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced

Replace By

SAE AMS6346B-2013

Latest

SAE AMS6346D-2023

Scope

This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars.

SAE AMS6346A-2009 history

• 2023 SAE AMS6346D-2023 Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Aircraft Quality Hardened and Tempered, 125 ksi (862 MPa) Tensile Strength
• 2018 SAE AMS6346C-2018 Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength
• 2013 SAE AMS6346B-2013 Steel Bars, 0.95Cr - 0.20Mo - (0.28 to 0.33C) (SAE 4130), Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength
• 2009 SAE AMS6346A-2009 Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength
• 2005 SAE AMS6346A-2005 Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength UNS G41300
• 1998 SAE AMS6346-1998 Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 ksi (862 MPa) Tensile Strength UNS G41300