Magnesium Alloy, Plate, Extra Flat 3.0Al – 1.0Zn – 0.20Mn (AZ31B-0) Annealed
- Aerospace Material Specification
- AMS4382D
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Sheet and Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-O) Annealed and Recrystallized |
| Aerospace Material Specification | Magnesium Alloy, Sheet and Plate 3.0Al - 1.0Zn – 0.20Mn (AZ31B-H24) Cold Rolled, Partially Annealed |
| Aerospace Material Specification | Aluminum Alloy, Plate (7449-T7951) 8.1Zn - 1.8Cu - 2.3Mg Solution Heat Treated, Stress Relieved, and Overaged |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| TABLE 1 | Composition | |
| TABLE 2 | Minimum Tensile Properties | |
| TABLE 3A | Thickness Tolerances, Inch/Pound Units | |
| TABLE 3B | Thickness Tolerances, SI Units | |
| TABLE 4A | Width or Length Tolerances, Inch/Pound Units | |
| TABLE 4B | Width or Length Tolerances, SI Units | |
| TABLE 5A | Lateral Bow Tolerances, Inch/Pound Units | |
| TABLE 5B | Lateral Bow Tolerances, SI Units | |
| TABLE 6A | Flatness Tolerances, Inch/Pound Units | |
| TABLE 6B | Flatness Tolerances, SI Units | |
| TABLE 7A | Squareness Tolerances: Maximum Allowable Difference in Length of Diagonals, Inch/Pound Units | |
| TABLE 7B | Squareness Tolerances: Maximum Allowable Difference in Length of Diagonals, SI Units |
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.