SAE International Alloy Bars and Forgings, Corrosion and Heat Resistant, 54ni 17.5cr 16.5co 4.0mo 2.9ti 2.9al 0.006b, Vacuum Melted, Solution Heat Treated AMS5753C

Description
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts, such as turbine blades, bolts, and fittings, requiring high strength up to 1600 degrees F (870 degrees Centigrade) and oxidation resistance up to 1800 degrees F (980 degrees C). This specification has been declared "Noncurrent" by the Aerospace materials Division, SAE, as of October 16, 1987. It is recommended, therefore, that this specification not be specified for new designs.
Description
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts, such as turbine blades, bolts, and fittings, requiring high strength up to 1600 degrees F (870 degrees Centigrade) and oxidation resistance up to 1800 degrees F (980 degrees C). This specification has been declared "Noncurrent" by the Aerospace materials Division, SAE, as of October 16, 1987. It is recommended, therefore, that this specification not be specified for new designs.

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Alloy Bars and Forgings, Corrosion and Heat Resistant, 54ni 17.5cr 16.5co 4.0mo 2.9ti 2.9al 0.006b, Vacuum Melted, Solution Heat Treated - AMS5753C - SAE International
Warrendale, PA, United States
Alloy Bars and Forgings, Corrosion and Heat Resistant, 54ni 17.5cr 16.5co 4.0mo 2.9ti 2.9al 0.006b, Vacuum Melted, Solution Heat Treated
AMS5753C
Alloy Bars and Forgings, Corrosion and Heat Resistant, 54ni 17.5cr 16.5co 4.0mo 2.9ti 2.9al 0.006b, Vacuum Melted, Solution Heat Treated AMS5753C
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts, such as turbine blades, bolts, and fittings, requiring high strength up to 1600 degrees F (870 degrees Centigrade) and oxidation resistance up to 1800 degrees F (980 degrees C). This specification has been declared "Noncurrent" by the Aerospace materials Division, SAE, as of October 16, 1987. It is recommended, therefore, that this specification not be specified for new designs.

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts, such as turbine blades, bolts, and fittings, requiring high strength up to 1600 degrees F (870 degrees Centigrade) and oxidation resistance up to 1800 degrees F (980 degrees C). This specification has been declared "Noncurrent" by the Aerospace materials Division, SAE, as of October 16, 1987. It is recommended, therefore, that this specification not be specified for new designs.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number AMS5753C
Product Name Alloy Bars and Forgings, Corrosion and Heat Resistant, 54ni 17.5cr 16.5co 4.0mo 2.9ti 2.9al 0.006b, Vacuum Melted, Solution Heat Treated
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