SAE AMS4474
Aluminum Alloy, Sheet and Plate, 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T8), Solution Heat Treated, Cold Worked, and Artificially Aged.
This product has been used typically for aerospace srructural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4474 | 2012-10-19 | Latest |