Aluminum Alloy Sheet, 2.7Cu - 2.2Li - 0.12Zr (2090-T83), Solution Heat Treated, Cold Worked, and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4251C
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Aluminum Alloy, Forgings, 4.3zn 3.3mg 0.6cu 0.2mn 0.2cr, Solution and Precipitation Heat Treated, Low Residual Stresses |
| Aerospace Material Specification | Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn; (2024-T861), Solution Heat Treated and Cold Worked, and Artificially Aged |
| Aerospace Standard | Test Method and Limits for Bow Height of Aluminum Sheet Samples After Chemical Milling |
Topic
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.