• SAE AMS4472

SAE AMS4472

  • Aluminum Alloy, Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T34) Solution Heat Treated and Stress Relieved
  • standard by SAE International, 06/06/2011
  • Category: SAE

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This specification covers an aluminum alloy in the form of plate.

This plate has been used typically for aerospace structural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications. Material is delivered in T34 temper and precipitation heat treated to obtain T82 temper by the end user.
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