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SAE AMS6325M : 2024

Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740), Heat Treated, 105 ksi (724 MPa) Tensile Strength

Standard Details

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

General Information

Status : ACTIVE
Standard Type: Main
Document No: SAE AMS6325M : 2024
Document Year: 2024
Pages: 8

Life Cycle

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SAE AMS6325M : 2024
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