• SAE AMS6325J

SAE AMS6325J

  • Steel, Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
  • standard by SAE International, 04/19/2010
  • Category: SAE

$81.00 $41.00

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, 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.
PDF

All of our standards document are available in PDF (Portable Document Format), an electronic, downloadable format.You will be able to download the file in your account downloads.

Multi-User Access

After purchasing, you have the ability to assign each license to a specific user.

Printable

At any time, you are permitted to make printed copies for your and your members' reference use.

Modern Engine Technology from A to Z
SAE AMS4899B

SAE AMS4899B

Titanium Alloy, Sheet, Strip, and Plate 4.5Al 3V 2Fe 2Mo Annealed..

$41.00 $81.00

SAE AMS4952D

SAE AMS4952D

Titanium Alloy, Welding Wire 6Al 2Sn 4Zr 2Mo..

$41.00 $81.00

SAE AMS4972F

SAE AMS4972F

Titanium Alloy, Bars, Wire, and Rings 8A1 1Mo 1V Solution Heat Treated and Stabilized..

$41.00 $81.00