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SAE AMS6327

Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength

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Organization: SAE
Publication Date: 1 September 2017
Status: active
Page Count: 8
scope:

Form

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

Application

These products have been used typically for parts, such as nuts, bolts, and screws, 1.50 inch (38.1 mm) and under in section thickness, requiring a minimum tensile strength of 125 ksi (862 MPa), but usage is not limited to such applications.

Document History

SAE AMS6327
September 1, 2017
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
Form This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings. Application These products have been used typically for parts, such as nuts, bolts, and...
October 1, 2012
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
Form This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings. Application These products have been used typically for parts, such as nuts, bolts, and...
October 1, 2007
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
Form This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings. Application These products have been used typically for parts, such as nuts, bolts, and...
January 1, 2003
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings. Application: These products have been used typically for parts, such as nuts, bolts, and screws,...
October 1, 1988
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125,000 psi (862 MPa) Tensile Strength
1. SCOPE: 1.1 Form: This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings. 1.2 Application: Primarily for parts, such as nuts, bolts, and screws, 1.50 inch...
January 15, 1981
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125, 000 psi (862 MPa) Tensile Strength
Form: This Specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings. Application: Primarily for parts, such as nuts, bolts, and screws, 1.50 in. (38 mm) and under in...
November 15, 1972
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125, 000 psi (862MPa) 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 screw, with sections...
September 30, 1966
STEEL BARS AND FORGINGS 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated (125, 000 psi Tensile)
APPLICATION: Primarily for parts, such as nuts, bolts, and screws, requiring a minimum tensile strength of 125, 000 psi.
June 1, 1951
STEEL 0.55Ni - 0.5Cr - 0.25Mo (0.38-0.43C) (SAE 8740) Heat Treated (125000TS)
A description is not available for this item.
July 1, 1945
STEEL .55 Ni - .5 Cr - .25 Mo (.38 - .43 C) Heat Treated (125,000 T.S.)
A description is not available for this item.
April 1, 1943
STEEL .55 Ni .5 Cr .25 Mo (.38 - .43 C) (125,000 T.S.)
A description is not available for this item.
September 1, 1942
STEEL .5 Ni .5 Cr .25 Mo (.38 - .43 C) (125,000 T.S.)
A description is not available for this item.

References

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