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)
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SAE AMS4252-1989
Standard No.
SAE AMS4252-1989
Release Date
1989
Published By
SAE - SAE International
Status
Be replaced
Replace By
SAE AMS4252A-1995
Latest
SAE AMS4252C-2018
Scope
Form: This specification covers an aluminium alloy in the form of plate. Application: Primarily for structural applications requiring a combination of high tensile strength and compressive properties and good exfoliation corrosion resistance.
SAE AMS4252-1989 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)
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