Aluminum Alloy, Alclad Sheet 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-0) Annealed, Fine Grain
- Aerospace Material Specification
- AMS4274A
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Aluminum Alloy Plate (2624-T351) 4.1Cu - 1.4Mg - 0.6Mn Solution Heat Treated, Cold Worked and Naturally Aged |
| 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 |
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1 | COMPOSITION, CORE (2024) | |
| TABLE 2 | COMPOSITION, CLADDING (1230) | |
| TABLE 3A | TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 3B | TENSILE PROPERTIES, SI UNITS | |
| TABLE 4 | BENDING PARAMETERS | |
| TABLE 5A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 5B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
| TABLE 6 | BENDING PARAMETERS | |
| TABLE 7 | MINIMUM AVERAGE 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.