Alloy Bars, Forgings, and Rings, Corrosion and Heat Resistant, 54ni - 17.5Cr - 16.5Co - 4.0Mo - 2.9Ti - 2.9Al - 0.006B, Solution, Stabilization, and Precipitation Heat Treated, Consumable Electrode or Vacuum Induction Melted(NONCURRENT Sep 2000)

Standard:
Reaffirmed:
  • 2012-04-12
 
  • HISTORICAL Access the latest revision: AMS5751F
Publisher:
  • SAE International
Pages:
8
Scope:

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. Primarily for parts, such as turbine components, requiring high strength up to 1600 degrees F (870 degrees C) and oxidation resistance up to 1800 degrees Farenheit (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.

Rationale:

AMS5751E has been reaffirmed to comply with the SAE five-year review policy.

History:
Standard Published Revision Status
AMS5751F 2017-04-06 Latest Stabilized
2012-04-12 Historical Reaffirmed
1994-04-01 Historical Reaffirmed
1981-04-01 Historical Revised
1974-12-01 Historical Revised
1964-06-01 Historical Revised
1960-06-01 Historical Issued
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