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Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.006B - 0.05Zr Consumable Electrode or Vacuum Induction Melted 1825 to 1900 °F Solution Heat Treated

  • Aerospace Material Specification
  • AMS5706M
  • Revised
Published January 14, 2015 by SAE International in United States
Digital Standard available
Downloadable datasets available
Annotation ability available
Language: English