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Aluminum Alloy, Rolled or Cold Finished Bars, Rods, and Wire 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73, T7351) Solution Heat Treated, Stress Relieved by Stretching, and Overaged

  • Aerospace Material Specification
  • AMS4124E
  • Revised
Published September 28, 2012 by SAE International in United States
Downloadable datasets available
Annotation ability available
Language: English