AMS6325K 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

12/20/2015

Features
Issuing Committee
Scope
Content
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
Rationale
Content
AMS6325K results from a Five Year Review and update of this specification that revises macrostructure, grain size testing, decarburization testing methods, and reporting.
Meta TagsDetails
DOI
https://doi.org/10.4271/AMS6325K
Pages
7
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 AMS6325K, Revised December 2015, Reaffirmed August 2000, Issued August 1942, https://doi.org/10.4271/AMS6325K.
Additional Details
Publisher
Published
Dec 20, 2015
Product Code
AMS6325K
Content Type
Material Specification
Status
Revised
Language
English