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ALLOY BARS AND FORGINGS, CORROSION AND HEAT RESISTANT Nickel Base - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al Consumable Electrode or Vacuum Induction Melted 1975 F (1079.4 C) Solution Heat Treated

  • Aerospace Material Specification
  • AMS5708A
  • Revised
Published May 01, 1970 by SAE International in United States
 
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Language: English