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About This Item

 

Full Description

This specification covers an aluminum alloy in the form of sheet.

This product has been used for aircraft applications where it offers a combination of high strength and low density, but usage is not limited to such applications.
 

Document History

  1. SAE AMS4412B


    Aluminum Alloy, Sheet 3.2Cu - 0.52Mg - 0.30Ag - 0.95 Li - 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged

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  2. SAE AMS4412A

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    Aluminum Alloy, Sheet 3.2Cu - 0.52Mg - 0.30Ag - 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged

    • Historical Version