Aluminum Alloy, Drawn, Round Seamless Tubing 2.5Mg - 0.25Cr (5052-0) Annealed
- Aerospace Material Specification
- AMS4070L
- Reaffirmed
Scope
Recommended Content
Aerospace Material Specification | Aluminum Alloy, Sheet and Plate 2.5Mg - 0.25Cr (5052-H32) Strain Hardened, Quarter-Hard, and Stabilized |
Aerospace Material Specification | Aluminum Alloy, Sheet and Plate 4.4Mg - 0.70Mn - 0.15Cr (5083-O) Annealed |
Aerospace Material Specification | Aluminum Alloy, Plate (7055-T7751) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr 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 2 | Tensile Properties | |
TABLE 3A | Minimum Flarability, Inch/Pound Units | |
TABLE 3B | Minimum Flarability, 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.