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SAE AMS6327
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SAE AMS6327 Revision L, September 1, 2017
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740)
Heat Treated, 125 ksi (862 MPa) Tensile Strength
Description / Abstract:
Form
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
Application
These products have been used typically for parts, such as nuts, bolts, and screws, 1.50 inch (38.1 mm) and under in section thickness, requiring a minimum tensile strength of 125 ksi (862 MPa), but usage is not limited to such applications.
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
Application
These products have been used typically for parts, such as nuts, bolts, and screws, 1.50 inch (38.1 mm) and under in section thickness, requiring a minimum tensile strength of 125 ksi (862 MPa), but usage is not limited to such applications.
SAE AMS6327 Revision L, September 1, 2017
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740)
Heat Treated, 125 ksi (862 MPa) Tensile Strength