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About This Item

 

Full Description

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

These products have been used typically for parts with sections 1.0 inch (25 mm) and under in nominal thickness requiring a minimum tensile strength of 125 ksi (862 MPa), but usage is not limited to such applications.
 

Document History

  1. SAE AMS6317L


    Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength

    • Most Recent
  2. SAE AMS6317K


    Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength

    • Historical Version
  3. SAE AMS6317J

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    Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength

    • Historical Version
  4. SAE AMS6317H


    Steel Bars and Forgings 1.8Ni 0.25Mo (0.38-0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength

    • Historical Version