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ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS, RODS, AND WIRE 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Overaged

  • Aerospace Material Specification
  • AMS4124C
  • Revised
Published April 01, 1997 by SAE International in United States
Downloadable datasets available
Annotation ability available
Language: English