SAE AMS6327J PDF

Name:
SAE AMS6327J PDF

Published Date:
10/01/2007

Status:
Active

Description:

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

Publisher:
SAE International

Document status:

Active

Format:

Electronic (PDF)

Delivery time:

10 minutes

Delivery time (for Russian version):

200 business days

SKU:

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.

File Size :	1 file , 460 KB
Note :	This product is unavailable in Ukraine, Russia, Belarus
Published :	10/01/2007

History

SAE AMS6327M

Published Date: 06/13/2024

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

$24.9

SAE AMS6327L

Published Date: 09/22/2017

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

$23.7

SAE AMS6327K

Published Date: 10/03/2012

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

$19.8

SAE AMS6327J

Published Date: 10/01/2007

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

$19.8

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SAE AMS6327J PDF

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

History

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