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SAE AMS4470

Aluminum Alloy, Plate (7085-T7451) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged

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Organization: SAE
Publication Date: 1 December 2018
Status: active
Page Count: 7
scope:

Form

This specification covers an aluminum alloy in the form of plate 3.000 to 7.000 inches (76.20 to 177.80 mm) in nominal thickness (see 8.5).

Application

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

 

Document History

SAE AMS4470
December 1, 2018
Aluminum Alloy, Plate (7085-T7451) 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 3.000 to 7.000 inches (76.20 to 177.80 mm) in nominal thickness (see 8.5). Application This product may be used in aerospace...
August 1, 2018
Aluminum Alloy, Plate (7085-T7451) 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 3.000 to 7.000 inches (76.20 to 177.80 mm) in nominal thickness (see 8.5). Application This product may be used in aerospace...
December 1, 2012
Aluminum Alloy, Plate (7085-T7451) 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 may be used in aerospace applications requiring a high level of mechanical properties and fracture...
October 1, 2009
Aluminum Alloy, Plate (7085-T7451) 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 may be used in aerospace applications requiring a high level of mechanical properties and fracture...

References

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