Aluminum Alloy, Extruded Profiles (2824-T3511), 4.0Cu - 1.35Mg - 0.7Mn, Solution Heat Treated and Stress Relieved by Stretching
- Aerospace Material Specification
- AMS4479A
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Aluminum Alloy, Extrusion 3.7Cu - 1.15Li - 0.5Zn - 0.45Ag - 0.4Mg - 0.3Mn - 0.1Zr (2055-T84) Solution Heat Treated, Stress Relieved by Stretching 2% to 5% and Aged |
Topic
Data Sets - Support Documents
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.
Reference
| Number | Title |
|---|---|
| AMS2355 | TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings |
| AMS2772 | HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
| ANSI H35.2 | This document is not part of the subscrption. |
| ANSI H35.2M | This document is not part of the subscrption. |
| APR823 | This document is not part of the subscrption. |
| AS1990 | ALUMINUM ALLOY TEMPERS |
| ASTMB594 | This document is not part of the subscrption. |
| ASTMB660 | This document is not part of the subscrption. |
| ASTMB666/B666M | This document is not part of the subscrption. |