SAE AMS5712H-2000
Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 53Ni 19Cr 11Co 9.8Mo 3.2Ti 1.6Al 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable

Standard No.

SAE AMS5712H-2000

Release Date

2000

Published By

Society of Automotive Engineers (SAE)

Status

Withdraw

Replace By

SAE AMS5712J-2006

Latest

SAE AMS5712L-2022

Scope

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts, such as turbine rotors, shafts,b bolts, dowels, and fittings, requiring high strength up (871 degrees C) after precipitation heat treatment and oxidation resistance up to 1800 degrees F (982 degrees C), but usage is not limited to such applications.

SAE AMS5712H-2000 history

• 2022 SAE AMS5712L-2022 Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable
• 2016 SAE AMS5712K-2016 Nickel Alloy@ Corrosion and Heat-Resistant@ Bars@ Forgings@ and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted@ Solution Heat Treated Precipitation Hardenable (UNS N07041)
• 2012 SAE AMS5712J-2012 Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable
• 2011 SAE AMS5712F-2011 ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated
• 2006 SAE AMS5712J-2006 Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable UNS N07041
• 2000 SAE AMS5712H-2000 Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 53Ni 19Cr 11Co 9.8Mo 3.2Ti 1.6Al 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable
• 1995 SAE AMS5712G-1995 Nickel Alloy@ Corrosion and Heat Resistant@ Bars@ Forgings@ and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted@ Solution Heat Treated Precipitation Hardenable (UNS N07041)
• 1985 SAE AMS5712E-1985 ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated
• 1983 SAE AMS5712D-1983 ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated
• 1977 SAE AMS5712C-1977 ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated
• 1966 SAE AMS5712B-1966 ALLOY, CORROSION AND HEAT RESISTANT Nickel Base - 19Cr - 11Co - 10Mo - 3Ti - 1.5Al Vacuum Melted, Solution Treated
• 1966 SAE AMS5712A-1966 ALLOY, CORROSION AND HEAT RESISTANT Nickel Base - 19Cr - 11Co - 10Mo - 3Ti - 1.5Al Vacuum Melted, Solution Treated
• 1960 SAE AMS5712-1960 ALLOY, CORROSION AND HEAT RESISTANT Nickel Base - 19Cr - 11Co - 10Mo - 3Ti - 1.5Al Vacuum Melted, Solution Treated