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
- Content
- This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
- Content
- AMS6325L results from a Five-Year Review and update of this specification that revises analytical methods (3.1), tempering of forgings (3.2.2), and macrostructure (3.4.1.1), prohibits unauthorized exceptions (3.7), and revises reporting and marking (4.4.1, 4.4.3, 5.2.1, 8.6).
- 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 AMS6325L, Revised April 2020, Reaffirmed August 2000, Issued August 1942, https://doi.org/10.4271/AMS6325L.