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Aluminum Alloy, Plate, 5.7Zn 2.2Mg 1.6Cu 0.22Cr (7475-T7351), Solution Heat Treated, Stress Relieved By Stretching, and Precipitation Heat Treated

  • Aerospace Material Specification
  • AMS4202A
  • Revised
Published July 01, 1981 by SAE International in United States
 
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Language: English