ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS, RODS, AND WIRE 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Overaged
- Aerospace Material Specification
Data Sets - Support Documents
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|TABLE 2||Minimum Tensile Properties|
|TABLE 3||Minimum Tensile Properties|
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.