Forgings, Magnesium Alloy, 2.0Th - 0.78Mn (HM21A - T5), Precipitation Heat Treated
- Aerospace Material Specification
|Aerospace Material Specification||Aluminum Alloy, Discontinuously Reinforced Hot Isostatically Pressed Shapes 2124A/SiC/25p (3μm) (T1P)|
|Aerospace Material Specification||Aluminum Alloy Extrusions 7.8Zn - 2.6Mg - 2.0Cu - 0.10Zr - (7068-T6511) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated|
|Aerospace Material Specification||Aluminum Alloy, Extruded Rod, Bar, and Profiles (7055-T76511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress-Relieved, and Overaged|
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.