SAE AMS5842D-2000
Cobalt-Nickel Alloy, Corrosion and Heat Resistant, Bars 19Cr 36Co 25Ni 7.0Mo 0.50Cb 2.9Ti 0.20Al 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened

Standard No.

SAE AMS5842D-2000

Release Date

2000

Published By

Society of Automotive Engineers (SAE)

Status

Withdraw

Replace By

SAE AMS5842E-2006

Latest

SAE AMS5842H-2022

Scope

This specification covers a high strength, corrosion and heat resistant cobalt-nickel-chromium alloy in the form of bars. These bars have been used typically for applications requiring a combination of high strength up to 1100 degrees F (593 degrees C), good tension-tension fatigue strength, toughness, and ductility, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice-corrosion, stress-corrosion cracking, and elevated temperature relaxation.

SAE AMS5842D-2000 history

• 2022 SAE AMS5842H-2022 Cobalt-Nickel Alloy, Corrosion- and Heat-Resistant, Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb (Nb) - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened
• 2016 SAE AMS5842G-2016 Cobalt-Nickel Alloy@ Corrosion and Heat-Resistant@ Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb (Nb) - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened (UNS R30159)
• 2011 SAE AMS5842F-2011 Cobalt-Nickel Alloy@ Corrosion and Heat-Resistant@ Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb (Nb) - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened (UNS R30159)
• 2006 SAE AMS5842E-2006 Cobalt-Nickel Alloy, Corrosion and Heat Resistant, Bars 19Cr - 36Co - 25Ni -7.0Mo - 0.50Cb - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened USN R30159
• 2000 SAE AMS5842D-2000 Cobalt-Nickel Alloy, Corrosion and Heat Resistant, Bars 19Cr 36Co 25Ni 7.0Mo 0.50Cb 2.9Ti 0.20Al 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened
• 1994 SAE AMS5842C-1994 Cobalt-Nickel Alloy@ Corrosion and Heat Resistant@ Bars 19Cr - 36Co - 25Ni -7.0Mo - 0.50Cb - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened (UNS R30159)
• 1988 SAE AMS5842B-1988 ALLOY BARS, CORROSION AND HEAT RESISTANT 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened
• 1983 SAE AMS5842A-1983 ALLOY BARS, CORROSION AND HEAT RESISTANT 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened
• 1977 SAE AMS5842-1977 ALLOY BARS, WORK STRENGTHENED, CORROSION AND HEAT RESISTANT 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb - 2.9Ti - 0.20Al - 9.0Fe Solution Heat Treated and Cold Drawn