ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS AND RODS 4.4Cu - 1.5Mg - 0.60Mn (2024-T851) Solution Heat Treated, Cold Worked, and Artificially Aged
- Aerospace Material Specification
- AMS4339
- Issued
Scope
Recommended Content
| Aerospace Material Specification | Aluminum Alloy Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075: (-T6 Sheet, -T651 Plate) Solution and Precipitation Heat Treated |
| Aerospace Material Specification | Aluminum Alloy, Sheet and Plate 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O) Annealed |
| Aerospace Material Specification | Aluminum Alloy Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024-T861) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2 | Minimum Tensile Properties |
Issuing Committee
AMS D Nonferrous Alloys Committee
The committee of Nonferrous Alloys, AMS Committee D, shall prepare, coordinate, and revise documents related to nonferrous metals technology, such as aluminum, magnesium, and copper, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.