Aluminum Alloy, Alclad Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075; -T76 Sheet, -T7651 Plate) Solution and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4316B
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Aluminum Alloy Bar, Rod, and Shapes, Extruded, 7075-T76 Improved Exfoliation Resistance |
| Aerospace Material Specification | Aluminum Sheet, Laminated Surface Bonded |
| Aerospace Material Specification | Aluminum Alloy, Sheet and Plate 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075: (-T76 Sheet, -T7651 Plate) Solution and Precipitation Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Table 1 | Composition, core (7075) | |
| Table 2 | Composition, cladding (7072) | |
| Table 3A | Minimum tensile properties, inch/pound units | |
| Table 3B | Minimum tensile properties, SI units | |
| Table 4 | Cladding thickness |
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.