SAE AMS4412A-2009
Aluminum Alloy@ Sheet 3.2Cu – 0.52Mg – 0.30Ag – 0.12Zr (2198-T8) Solution Heat Treated@ Cold Worked@ and Artificially Aged (UNS A92198)
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SAE AMS4412A-2009
Standard No.
SAE AMS4412A-2009
Release Date
2009
Published By
SAE - SAE International
Status
Be replaced
Replace By
SAE AMS4412A-2015
Latest
SAE AMS4412B-2021
Scope
Form This specification covers an aluminum alloy in the form of sheet. Application This product has been used for aircraft applications where if offers a combination of high strength and low density@ but usage is not limited to such applications.
SAE AMS4412A-2009 history
2021
SAE AMS4412B-2021
Aluminum Alloy, Sheet 3.2Cu - 0.52Mg - 0.30Ag - 0.95 Li - 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged (UNS A92198)
2015
SAE AMS4412A-2015
Aluminum Alloy, Sheet 3.2Cu - 0.52Mg - 0.30Ag - 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged
2009
SAE AMS4412A-2009
Aluminum Alloy@ Sheet 3.2Cu – 0.52Mg – 0.30Ag – 0.12Zr (2198-T8) Solution Heat Treated@ Cold Worked@ and Artificially Aged (UNS A92198)
2007
SAE AMS4412-2007
Aluminum Alloy, Sheet, 3.2Cu 0.52Mg 0.30Ag 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged
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