Aluminum Bronze, Bars, Rods, Shapes, Tubes, and Forgings 81.5Cu - 10.0Al - 4.8Ni - 3.0Fe Drawn and Stress Relieved (HR50) or Temper Annealed (TQ50)
- Aerospace Material Specification
- AMS4640G
- Revised
Scope
Recommended Content
Aerospace Material Specification | Leaded Brass, Seamless Tubing 66.5Cu - 32.5Zn - 0.48Pb Light Annealed (O50) |
Aerospace Material Specification | Brass, Naval, Bars and Rods 60.5Cu - 38.7Zn - 0.8Sn Half Hard (H02) |
Aerospace Material Specification | Bronze, Aluminum Silicon, Rods, Bars, and Forgings 90Cu - 7.0Al - 1.8Si Drawn and Stress Relieved (HR50) |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | Composition | |
TABLE 2A | Minimum Tensile Properties, Inch/Pound Units | |
TABLE 3A | Minimum Tensile Properties, Inch/Pound Units | |
TABLE 3B | Minimum Tensile Properties, SI Units | |
TABLE 4 | Hardness | |
TABLE 5 | Hardness |
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.