SAE AMS6370
Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
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| Organization: | SAE |
| Publication Date: | 1 July 2020 |
| Status: | active |
| Page Count: | 8 |
scope:
Form
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
Application
These products have been used typically for parts, 0.50 inch (12.7 mm) and under in section thickness at time of heat treatment, requiring a through-hardened steel capable of developing hardness as high as 35 HRC when hardened and tempered, and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
Document History
SAE AMS6370
July 1, 2020
Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
Form
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
Application
These products have...
February 1, 2016
Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
Form
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
Application
These products have...
May 1, 2011
Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
Form
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
Application
These products have...
May 1, 2006
Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
Form
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
Application
These products have...
October 1, 2001
Steel, Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
SCOPE: Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. Application: These products...
October 1, 1990
Steel Bars, Forgings, and Rings 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
1. SCOPE: 1.1 Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. 1.2 Application:...
October 1, 1983
STEEL BARS, FORGINGS, AND RINGS 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
Form: This Specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging and flash welded rings.
Application: Primarily for parts...
July 1, 1976
STEEL BARS, FORGINGS, AND RINGS 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
Form: This Specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging and flash welded rings.
Application: Primarily for parts...
November 15, 1971
STEEL BARS, FORGINGS AND RINGS 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
Form: This Specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging and flash welded rings.
Application: Primarily for parts...
May 1, 1970
STEEL BARS, FORGINGS AND RINGS 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
APPLICATION: Primarily for parts with sections 0.50 in. or less in thickness at the time of heat treatment which require a through-hardening steel capable of developing hardness as high as Rockwell C...
October 1, 1951
STEEL BARS AND FORGINGS 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130)
APPLICATION: Parts with sections 0.50 in. or less in thickness at the time of heat treatment which require a through-hardening steel capable of developing hardness as high as Rockwell C 35 when...
October 1, 1951
STEEL 0.95Cr - 0.2Mo (0.28-0.33C) (SAE 4130)
APPLICATION: Parts with sections 0.50 in. or less in thickness at the time of heat treatment which require a through-hardening steel capable of developing hardness as high as Rockwell C 35 when...
March 1, 1949
STEEL 0.95Cr - 0.2Mo (0.27-0.33C) (SAE 4130)
APPLICATION: Parts with sections 0.50 in. or less in thickness which require a through-hardening steel capable of developing hardness of Rockwell C 35 when properly hardened and tempered and also...
January 1, 1946
STEEL .95Cr .2 Mo (.27-.33 C)
A description is not available for this item.
March 1, 1942
STEEL Chromium Molybdenum .27 - .33 Carbon
A description is not available for this item.
December 4, 1939
STEEL Chromium Molybdenum
A description is not available for this item.