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ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 41.5Ni - 16Cr - 37Fe - 2.9Cb - 1.8Ti Consumable Electrode or Vacuum Induction Melted 1800°F (980°C) Solution Heat Treated

  • Aerospace Material Specification
  • AMS5701A
  • Revised
Published April 01, 1981 by SAE International in United States
Annotation ability available
Language: English