AMS6325M: 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 - Material Specification

Issuing Committee: AMS E Carbon and Low Alloy Steels Committee

Scope

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

Meta Tags

Topics: Materials properties
Tensile strength
Heat treatment
Steel
Aircraft
Forging

Details

DOI: https://doi.org/10.4271/AMS6325M

Pages: 8

Citation: SAE International Material Specification, 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, SAE Standard AMS6325M, Revised December 2024, Issued September 1942, https://doi.org/10.4271/AMS6325M.

Additional Details

Publisher: SAE International

Published: Dec 18

Product Code: AMS6325M

Content Type: Material Specification

Status: Revised

Language: English

Historical