ALUMINUM ALLOY, EXTRUSIONS 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged
- Aerospace Material Specification
- AMS4167G
- Revised
Scope
Recommended Content
Aerospace Material Specification | Aluminum Alloy Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3) Solution Heat Treated and Cold Worked |
Aerospace Material Specification | Magnesium Alloy, Extrusions 5.5Zn - 0.45Zr (ZK60A-T5) Precipitation Heat Treated |
Aerospace Material Specification | Aluminum Alloy Extrusions 7.8Zn - 2.6Mg - 2.0Cu - 0.10Zr - (7068-T6511) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | Composition | |
TABLE 2A | Minimum Longitudinal Tensile Properties, Inch/Pound Units | |
TABLE 2B | Minimum Longitudinal Tensile Properties, SI Units | |
TABLE 3A | Minimum Long-Transverse Tensile Properties, Inch/Pound Units | |
TABLE 38 | Minimum Long-Transverse Tensile Properties, SI Units | |
TABLE 4A | Minimum Short-Transverse Tensile Properties, Inch/Pound Units | |
TABLE 4B | Minimum Short-Transverse Tensile Properties, SI Units |
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.