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About This Item

 

Full Description

This specification covers an aluminum alloy in the form of plate products from 1.000 to 6.000 inches (152.40 mm) in thickness.

7065-T7451 may be used in aerospace applications requiring high strength and fracture toughness, high resistance to stress-corrosion cracking and good resistance to exfoliation corrosion, but usage is not limited to such applications.

 

Document History

  1. SAE AMS4361A


    Aluminum Alloy, Plate (7065-T7451) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

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  2. SAE AMS4361

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    Aluminum Alloy, Plate (7065-T7451) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

    • Historical Version