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SAE AMS4329

Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged

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Organization: SAE
Publication Date: 1 October 2017
Status: active
Page Count: 6
scope:

Form

This specification covers an aluminum alloy in the form of plate 4.001 to 7.000 inch, incl. (101.62 to 177.80 mm, incl.) in thickness.

Application

This product has been used in aerospace applications requiring a high level of mechanical properties and fracture toughness, moderate resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.

Document History

SAE AMS4329
October 1, 2017
Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
Form This specification covers an aluminum alloy in the form of plate 4.001 to 7.000 inch, incl. (101.62 to 177.80 mm, incl.) in thickness. Application This product has been used in aerospace...
May 1, 2006
Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
Form This specification covers an aluminum alloy in the form of plate. Application This product has been used in aerospace applications requiring a high level of mechanical properties and fracture...
May 1, 2006
Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
Form This specification covers an aluminum alloy in the form of plate. Application This product has been used in aerospace applications requiring a high level of mechanical properties and fracture...
July 1, 2003
Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
Form: This specification covers an aluminum alloy in the form of plate. Application: This product has been used in aerospace applications requiring a high level of mechanical properties, moderate...

References

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