ALUMINUM ALLOY SHEET AND PLATE 2.5Mg - 0.25Cr (5052-H34) Strain-Hardened, Half-Hard, and Stabilized
- Aerospace Material Specification
- AMS4017J
- Revised
Scope
Recommended Content
| Aerospace Material Specification | Aluminum Alloy, Bars, Rods, and Wire, Rolled Or Cold-Finished 99.0a1, as Fabricated |
| Aerospace Material Specification | Aluminum Alloy Sheet, Alclad 6.0Cu - 0.40Zr - (2004-F) As Rolled |
| Aerospace Material Specification | Aluminum Sheet and Plate, 0.12Cu (1100-0), Annealed |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Tensile Properties, Inch/Pound Units | |
| TABLE 2B | Tensile Properties, SI Units | |
| TABLE 3 | Bending Requirements |
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.