SAE International Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength AMS6325M

Description
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings.
Description
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings.

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Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength - AMS6325M - SAE International
Warrendale, PA, United States
Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
AMS6325M
Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength AMS6325M
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings.

This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number AMS6325M
Product Name Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
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