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ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 52.5Ni - 19Cr - 3.0Mo - 5.1(Cb+Ta) - 0.90Ti - 0.50Al - 19Fe Consumable Electrode or Vacuum Induction Melted 1950°F (1066°C) Solution Heat Treated, Precipitation Hardenable

  • Aerospace Material Specification
  • AMS5664C
  • Revised
Published October 01, 1990 by SAE International in United States
Downloadable datasets available
Annotation ability available
Language: English