HEAT TREATMENT OF ALUMINUM AND ALUMINUM ALLOYS
- Aerospace Material Specification
- AMS2770A
- Revised
Scope
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
TABLE I | ||
TABLE II | ANNEALING OF WROUGHT ALUMINUM AND ALUMINUM ALLOYS | |
TABLE III | MAXIMUM THICKNESS AT TIME OF SOLUTION HEAT TREATMENT | |
TABLE IV | SOLUTION HEAT TREAT SOAK TIME AND PERMISSIBLE QUENCH DELAY | |
TABLE V | SOLUTION HEAT TREATMENT | |
TABLE VI | PRECIPITATION HEAT TREATMENT | |
TABLE VI | (Continued) | |
TABLE VI | (Continued) |
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.
Reference
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