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
|Aerospace Material Specification||Aluminum Alloy, Forgings and Rolled or Forged Rings (6061-T6) Solution and Precipitation Heat Treated|
|Aerospace Material Specification||Aluminum Alloy Forgings and Rolled or Forged Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally Aged|
|Aerospace Material Specification||Aluminum Alloy, Rolled or Cold Finished Bars and Rods, 12.2Si - 1.0Mg - 0.90Cu - 0.90Ni (4032-T86) Solution Heat Treated, Cold Worked, and Artificially Aged|
Data Sets - Support Documents
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.