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About This Item

 

Full Description

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

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 125,000 (862 MPa) but usage is not limited to such applications.
 

Document History

  1. SAE AMS6327L


    Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength

    • Most Recent
  2. SAE AMS6327K


    Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength

    • Historical Version
  3. SAE AMS6327J

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    Steel Bars and Forgings 0.50Cr 0.55Ni 0.25Mo (0.38 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength

    • Historical Version