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ALUMINUM ALLOY EXTRUSIONS 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated and Stress-Relieved by Stretching

  • Aerospace Material Specification
  • AMS4163A
  • Revised
Published January 01, 1977 by SAE International in United States
 
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Language: English