Magnesium Alloy, Sheet and Plate, 2.0Th - 0.78Mn, Solution Heat Treated, Cold Worked, and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4383F
- Cancelled
Scope
Rationale
Recommended Content
Aerospace Material Specification | Aluminum Alloy, Rolled or Forged Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T651, 6061-T652) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated |
Aerospace Material Specification | Forgings, Magnesium Alloy, 2.0Th - 0.78Mn (HM21A - T5), Precipitation Heat Treated |
Aerospace Material Specification | Magnesium Alloy, Sheet and Plate, 3.2Th - 0.70Zr, Cold Rolled and Partially Annealed |
Data Sets - Support Documents
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.