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SAE AMS6325

Steel, Bars, and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength

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

Form

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

Application

These products have been used typically for parts, such as nuts, bolts, and screws, 1.750 inches (44.45 mm) and under in section thickness requiring a minimum tensile strength of 105 ksi (724 MPa), but usage is not limited to such applications.

Document History

SAE AMS6325
April 1, 2020
Steel, Bars, and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
Form This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings. Application These products have been used typically for parts, such as nuts,...
December 1, 2015
Steel, Bars, and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
Form This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings. Application These products have been used typically for parts, such as nuts,...
April 1, 2010
Steel, Bars and Forgings 0.50Cr – 0.55Ni – 0.25Mo (0.38 – 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
Form This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings. Application These products have been used typically for parts, such as nuts,...
October 1, 2004
Steel, Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength
Form: This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings. Application: These products have been used typically for parts, such as nuts,...
May 1, 1994
Steel, Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength (UNS G87400)
1. SCOPE: 1.1 Form: This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings. 1.2 Application: These products have been used typically for parts,...
July 1, 1988
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105, 000 psi (724 MPa) Tensile Strength
Form: This specification covers an aircraft quality, low-alloy steel in the form of heat treated bars and forgings. Application: Primarily for parts, such as nuts, bolts, and screws, 1.750 inches...
November 15, 1972
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105, 000 psi (724 MPa) Tensile Strength
Form: This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings. Application: Primarily for parts, such as nuts, bolts, and screws, with sections...
September 30, 1966
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated (105, 000 psi Tensile)
APPLICATION: Primarily for parts, such as nuts, bolts, and screws, requiring a minimum tensile strength of 105, 000 psi.
June 1, 1951
STEEL 0.55Ni - 0.5Cr - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated (105000TS)
A description is not available for this item.
July 1, 1945
STEEL .55 Ni .5 Cr .25 Mo (.38 - .43 C) Heat Treated (105,000 TS)
A description is not available for this item.
April 1, 1943
STEEL .55 Ni .5 Cr .25 Mo (.38-.43 C) (105,000 TS)
A description is not available for this item.
September 1, 1942
STEEL .5 Ni .5 Cr .25 Mo (.38-.43 C) (105,000 TS)
A description is not available for this item.

References

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