Aluminum Alloy, Die Forgings, 5.6zn 2.5mg 1.6cu 0.23cr Solution and Precipitation Heat Treated
- Aerospace Material Specification
|Aerospace Material Specification||Aluminum Alloy Die Forgings 4.0Cu - 2.0Ni - 0.68Mg (2018-T61) Solution and Precipitation Heat Treated|
|Aerospace Material Specification||Titanium Alloy, Forgings 10V - 2Fe - 3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Aged 180 ksi (1241 MPa) Tensile Strength|
|Aerospace Material Specification||Heat Treatment of Aluminum Alloy Raw Materials|
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.