AMS4413C Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged
Revised
12/20/2023
- Features
- Issuing Committee
- Content
- This specification covers an aluminum-lithium alloy in the form of plate 0.500 to 8.000 inches (12.70 to 203.20 mm), inclusive, in thickness (see 8.5).
- Content
- AMS4413C results from an update of this specification with changes to increase the maximum product thickness to 8.000 inches (203.20 mm) (see 1.1, Table 2, and Table 3), update SI unit elongation values for consistency with AMS editorial guidalines (see Table 2B), remove S-L fracture toughness from 0.50- to 1.500-inch (12.50- to 38.20-mm), inclusive, thick product because the specimen is not supported (see Table 3), update wording to prohibit unauthorized exceptions (see 3.3.4, 4.4.1, and 8.3), Applicable Documents (see Section 2), Ordering Information (see 8.5), and relocate Definitions (see 2.4).
- Pages
- 7
- Citation
- SAE International Material Specification, Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged, SAE Standard AMS4413C, Revised December 2023, Issued October 2007, https://doi.org/10.4271/AMS4413C.