SAE AMS 4412A

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SAE AMS 4412A English Secure PDF Aluminum Alloy, Sheet, 3.2Cu 0.52Mg 0.30Ag 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged

standard published 05/15/2009 by SAE International

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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.