Aluminum-Alloy Castings, High Strength
- Aerospace Material Specification
- AMSA21180C
- Stabilized
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Aluminum Alloy Castings 7.0Si - 0.55Mg - 0.12Ti - 0.06Be (A357.0 T6) Solution and Precipitation Heat Treated |
| Aerospace Material Specification | Aluminum Alloy Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated |
Topic
Data Sets - Support Documents
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| TABLE 1 | CHEMICAL COMPOSITION | |
| TABLE 2 | MAXIMUM ACCEPTABLE DISCONTINUITIES IN ALUMINUM-ALLOY CASTINGS (MAXIMUM PERMISSIBLE RADIOGRAPH IN ACCORDANCE WITH ASTM E 155) , , , | |
| TABLE 3 | MECHANICAL PROPERTIES OF SPECIMENS CUT FROM DESIGNATED AREAS OF CASTINGS (SEE ) , | |
| TABLE 4 | MECHANICAL PROPERTIES OF SPECIMENS CUT FROM ANY AREA OF CASTING (SEE ) , | |
| TABLE 5 | SOLUTION HEAT-TREATING CONDITIONS | |
| TABLE 6 | AGING (PRECIPITATION) HEAT TREATMENTS | |
| TABLE 7 | INSPECTION SAMPLING PLAN |
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.