SAE AMS6346A PDF

SAE AMS6346A PDF

Name:
SAE AMS6346A PDF

Published Date:
09/22/2005

Status:
Active

Description:

Steel Bars, 0.95Cr - 0.20Mo - (0.28 to 0.33C) (SAE 4130), Hardened and Tempered, 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

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Choose Document Language:
$21
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This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars.

These bars have been used typically for parts with sections 1.50 inch (38.100 mm) and under in nominal thickness requiring a minimum tensile strength of 125 ksi (863 MPa), but usage is not limited to such application.
File Size : 1 file , 240 KB
Note : This product is unavailable in Ukraine, Russia, Belarus
Published : 09/22/2005

History

SAE AMS6346D
Published Date: 10/16/2023
Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Aircraft Quality Hardened and Tempered, 125 ksi (862 MPa) Tensile Strength
$23.7
SAE AMS6346C
Published Date: 06/11/2018
Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength
$19.8
SAE AMS6346B
Published Date: 10/04/2013
Steel Bars 0.95Cr - 0.20Mo (0.28 to 0.33C) (SAE 4130) Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength
$18.3
SAE AMS6346A
Published Date: 09/22/2005
Steel Bars, 0.95Cr - 0.20Mo - (0.28 to 0.33C) (SAE 4130), Hardened and Tempered, 125 Ksi (862 MPa) Tensile Strength
$21

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