Aluminum Alloy, Rolled or Forged Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T651, 6061-T652) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4312E
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Aluminum Alloy Forgings and Rolled or Forged Rings and Forging Stock 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally Aged |
Aerospace Material Specification | Aluminum Alloy, Forgings and Rolled or Forged Rings (6061-T6) Solution and Precipitation Heat Treated |
Aerospace Material Specification | Aluminum Alloy 3003, Bar, Rod, Shapes, Tube, and Wire, Extruded |
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.
Reference
Number | Title |
---|---|
AMS2355 | TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings |
AMS2772 | HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
ASTMB594 | This document is not part of the subscrption. |
ASTMB660 | This document is not part of the subscrption. |
ASTMB666/B666M | This document is not part of the subscrption. |