AMS6325A 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
04/01/1943
- Issuing Committee
- Content
- This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
- Pages
- 2
- 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 AMS6325A, Revised April 1943, Issued September 1942, https://doi.org/10.4271/AMS6325A.