Aluminum Alloy Plate (7081-T7451) 7.2Zn - 1.5Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved and Overaged
- Aerospace Material Specification
- AMS4410A
- Stabilized
Scope
Rationale
Recommended Content
Topic
Data Sets - Support Documents
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| TABLE 1 | COMPOSITION | |
| TABLE 2A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 2B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
| TABLE 3 | MINIMUM FRACTURE TOUGHNESS PARAMETERS |
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
| Number | Title |
|---|---|
| AMS2355 | TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings |
| AMS2772 | HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
| AS1990 | Aluminum Alloy Tempers |
| AS1990A | ALUMINUM ALLOY TEMPERS |
| ASTMB557 | This document is not part of the subscrption. |
| ASTMB594 | This document is not part of the subscrption. |
| ASTMB645 | This document is not part of the subscrption. |
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| ASTMB666/B666M | This document is not part of the subscrption. |
| ASTME399 | This document is not part of the subscrption. |
| ASTMG34 | This document is not part of the subscrption. |
| ASTMG47 | This document is not part of the subscrption. |