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SAE AMS6412

Steel, Bars and Forgings 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)

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Organization: SAE
Publication Date: 1 October 2020
Status: active
Page Count: 8
scope:

Form

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.

Application

These products have been used typically for parts, 0.875 inch (22.22 mm) and under in nominal section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 50 HRC and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

Document History

SAE AMS6412
October 1, 2020
Steel, Bars and Forgings 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application These products have been used typically for parts, 0.875 inch...
December 1, 2015
Steel, Bars and Forgings 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application These products have been used typically for parts, 0.875 inch...
May 1, 2010
Steel, Bars and Forgings 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application These products have been used typically for parts, 0.875 inch...
July 1, 2001
Steel, Bars and Forgings 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application: These products have been used typically for parts, 0.875 inch...
July 1, 2001
Steel, Bars and Forgings 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application: These products have been used typically for parts, 0.875 inch...
December 1, 1994
Steel, Bars and Forgings 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337) (UNS G43370)
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. These products have been used typically for parts, 0.875 inch (22.22 mm) and under in...
October 1, 1989
STEEL BARS AND FORGINGS 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application: Primarily for parts, 0.875 inch (22.22 mm) and under in nominal...
April 15, 1980
STEEL BARS AND FORGINGS 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application: Primarily for parts with sections 0.875 in. (22 mm) and under in...
November 15, 1971
STEEL BARS AND FORGINGS 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Application: Primarily for parts with sections 0.875 in. (22.225 mm) or less in...
November 1, 1967
STEEL BARS AND FORGINGS 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
APPLICATION: Parts with sections 0.875 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 50 when...
January 31, 1964
STEEL BARS AND FORGINGS 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)
APPLICATION: Parts with sections 0.875 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 50 when...
June 1, 1951
STEEL 1.8Ni - 0.8Cr - 0.25Mo (0.35-0.40C) (4337)
APPLICATION: Parts with sections 0.875 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 50 when...
December 1, 1950
STEEL 1.8Ni - 0.8Cr - 0.25Mo (0.35-0.40C) (4337)
APPLICATION: Parts with sections 0.875 in. or less in thickness at the time of heat treatment which require a through-hardening steel capable of developing hardness of Rockwell C50 when properly...
August 1, 1945
STEEL 1.8 Ni .8 Cr .25 Mo (.35-.40C)
A description is not available for this item.
March 1, 1942
STEEL Nickel Chromium Molybdenum
A description is not available for this item.
January 23, 1940
STEEL Nickel Chromium Molybdenum
A description is not available for this item.

References

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