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SAE AMS6320

Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (8735)

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Organization: SAE
Publication Date: 1 October 2017
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, 0.75 inch (19.0 mm) and under in nominal section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionally lower hardness, but usage is not limited to such applications.

Document History

SAE AMS6320
October 1, 2017
Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (8735)
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...
September 1, 2012
Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (8735)
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...
November 1, 2007
Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735)
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...
January 1, 2003
Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735)
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...
January 1, 1990
Steel Bars, Forgings, and Rings 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735)
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, 1989
STEEL BARS, FORGINGS, AND RINGS 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735)
Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forging, flash welded rings, and stock for forging or flash welded rings. Application: Primarily for parts,...
July 1, 1981
STEEL BARS, FORGINGS, AND RINGS 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735)
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: Primarily for parts...
November 1, 1967
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735)
APPLICATION: Primarily for parts with section 0.75 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...
November 1, 1967
STEEL BARS, FORGINGS, AND RINGS 0.50Cr - 0.55Ni - 0.25Mo (0.33 - 0.38C) (SAE 8735)
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...
January 31, 1964
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.33-0.38C) (SAE 8735)
APPLICATION: Parts with sections 0.75 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 40 when...
June 1, 1951
STEEL 0.55Ni - 0.5Cr - 0.25Mo (0.33-0.38C) (SAE 8735)
APPLICATION: Parts with sections 0.75 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 40 when...
December 1, 1950
Steel 0.55Ni - 0.5Cr - 0.25Mo (0.33-0.38C) (SAE 8735)
APPLICATION: Parts with sections 0.75 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 C40 when...
August 1, 1945
STEEL .55 Ni .5 Cr .25 Mo (.33-.38C)
A description is not available for this item.
April 1, 1943
STEEL .55 Ni .5 Cr .25 Mo (.33-.38 C)
A description is not available for this item.
September 1, 1942
STEEL .5Ni .5Cr .25Mo (.33-.38 C)
A description is not available for this item.

References

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