Aluminum Alloy, Plate 4.4Cu - 1.5Mg - 0.60Mn (2124-T851) Solution Heat Treated, Stretched, and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4101E
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Aluminum Alloy, Plate 4.4Cu - 1.5Mg - 0.60Mn (2124-T851) Solution Heat Treated, Stretched, and Precipitation Heat Treated |
| Aerospace Material Specification | Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn; (2024-T861), Solution Heat Treated and Cold Worked, and Artificially Aged |
| Aerospace Material Specification | Aluminum Alloy, Plate (7255-T7751) 8.0Zn - 2.3Cu - 2.0Mg - 0.12Zr Solution Heat Treated, Stress Relieved, and Overaged |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 2B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
| TABLE 3 | MINIMUM FRACTURE TOUGHNESS VALUES |
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.