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SAE AMS6325

Revision K, December 1, 2015

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



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Product Details:

  • Revision: Revision K, December 1, 2015
  • Published Date: December 2015
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 7
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form

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

Application

These products have been used typically for parts, such as nuts, bolts, and screws, 1.750 inches (44.45 mm) and under in section thickness requiring a minimum tensile strength of 105 ksi (724 MPa), but usage is not limited to such applications.
AIA/NAS Aerospace Standards