SAE AMS4412A
Aluminum Alloy, Sheet, 3.2Cu - 0.52Mg - 0.30Ag - 0.12Zr (2198-T8), Solution Heat Treated, Cold Worked, and Artificially Aged.
This specification covers an aluminum alloy in the form of sheet.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.
History:Standard | Published | Revision | Status |
---|---|---|---|
AMS4412A | 2009-05-15 | Latest | |
AMS4412 | 2007-11-21 | Historical |