Aluminum Alloy Forgings, Heat Treated
- Aerospace Material Specification
- AMSA22771D
- Stabilized
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Aluminum Alloy Forgings |
| Aerospace Material Specification | Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
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| TABLE 1 | CHEMICAL COMPOSITION , | |
| TABLE 2 | MECHANICAL PROPERTIES OF DIE FORGINGS, SPECIMEN AXIS PARALLEL TO DIRECTION OF GRAIN FLOW LINES | |
| TABLE 3 | MECHANICAL PROPERTIES OF DIE FORGINGS, SPECIMEN AXIS NOT PARALLEL TO DIRECTION OF GRAIN FLOW LINES | |
| TABLE 4 | MECHANICAL PROPERTIES OF HAND FORGINGS , | |
| TABLE 5 | MECHANICAL PROPERTIES OF ROLLED RING FORGINGS , | |
| TABLE 6 | RECOMMENDED BRINELL HARDNESS (MINIMUM) |
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.