SAE AMS4329-2003
Aluminum Alloy, Plate (7085-T7651) 7.5Zn 1.6Cu 1.5Mg 0.12ZrSolution Heat Treated, Stress-Relieved, and Overaged

Standard No.
SAE AMS4329-2003
Release Date
2003
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4329A-2006
Latest
SAE AMS4329B-2017
Scope
This specification covers an aluminum alloy in the form ofplate. This product has been used in aerospace applicationsrequiring a high level of mechanical properties, moderateresistance stress-corrosion cracking and resistance toexfoliation corrosion, but usage is not limited to suchapplications.

SAE AMS4329-2003 history

  • 2017 SAE AMS4329B-2017 Aluminum Alloy@ Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated@ Stress-Relieved@ and Overaged (UNS A97085)
  • 2011 SAE AMS4329A-2011 Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
  • 2006 SAE AMS4329A-2006 Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged UNS A97085
  • 2003 SAE AMS4329-2003 Aluminum Alloy, Plate (7085-T7651) 7.5Zn 1.6Cu 1.5Mg 0.12ZrSolution Heat Treated, Stress-Relieved, and Overaged



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