AMS6325L Steel, Bars, and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength

Revised

04/10/2020

Features
Issuing Committee
Scope
Content
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
Meta TagsDetails
DOI
https://doi.org/10.4271/AMS6325L
Pages
8
Citation
SAE International Material Specification, Steel, Bars, and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength, SAE Standard AMS6325L, Revised April 2020, Reaffirmed August 2000, Issued August 1942, https://doi.org/10.4271/AMS6325L.
Additional Details
Publisher
Published
Apr 10, 2020
Product Code
AMS6325L
Content Type
Material Specification
Status
Revised
Language
English