SAE AMS4252C-2018
Aluminum Alloy@ Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated@ Stress Relieved@ and Overaged (UNS A97150)

Standard No.
SAE AMS4252C-2018
Release Date
2018
Published By
SAE - SAE International
Latest
SAE AMS4252C-2018
Scope
Form This specification covers an aluminum alloy in the form of plate 0.250 to 3.000 inch (6.35 to 76.20 mm) inclusive@ in nominal thickness (see 8.7). Application This plate has been used typically for structural applications requiring a combination of high tensile strength and compressive properties and good exfoliation corrosion resistance@ but usage is not limited to such applications.

SAE AMS4252C-2018 history

  • 2018 SAE AMS4252C-2018 Aluminum Alloy@ Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated@ Stress Relieved@ and Overaged (UNS A97150)
  • 2012 SAE AMS4252B-2012 Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged
  • 2005 SAE AMS4252B-2005 Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged UNS A97150
  • 1995 SAE AMS4252A-1995 Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged (UNS A97150)
  • 1989 SAE AMS4252-1989 ALUMINUM ALLOY PLATE 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated@ Stress Relieved@ and Overaged (UNS A97150)
Aluminum Alloy@ Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated@ Stress Relieved@ and Overaged (UNS A97150)



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