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SAE AMS4252

Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged

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Organization: SAE
Publication Date: 1 June 2018
Status: active
Page Count: 7
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.

Document History

SAE AMS4252
June 1, 2018
Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged
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...
March 1, 2005
Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged
Form: This specification covers an aluminum alloy in the form of plate. Application: This plate has been used typically for structural applications requiring a combination of high tensile strength...
March 1, 2005
Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged
Form: This specification covers an aluminum alloy in the form of plate. Application: This plate has been used typically for structural applications requiring a combination of high tensile strength...
March 1, 1995
Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged (UNS A97150)
SCOPE: Form: This specification covers an aluminum alloy in the form of plate. Application: This plate has been used typically for structural applications requiring a combination of high tensile...
October 1, 1989
ALUMINUM ALLOY PLATE 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T7751) Solution Heat Treated, Stress Relieved, and Overaged
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...

References

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