SAE AMS4412-2007
Aluminum Alloy, Sheet, 3.2Cu 0.52Mg 0.30Ag 0.12Zr (2198-T8) Solution Heat Treated, Cold Worked, and Artificially Aged

Standard No.

SAE AMS4412-2007

Release Date

2007

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced 2015-03

Replace By

SAE AMS4412A-2009

Latest

SAE AMS4412B-2021

Scope

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.

SAE AMS4412-2007 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