AMS6325J 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
04/19/2010
- Features
- Issuing Committee
- Content
- This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
- Content
- AMS6325J results from a Five Year Review and update of this specification.
- Pages
- 1
- 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 AMS6325J, Revised April 2010, Reaffirmed August 2000, Issued August 1942, https://doi.org/10.4271/AMS6325J.