Titanium Alloy Bars, Wire, and Forgings 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo Solution and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4981E
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated |
| Aerospace Material Specification | Titanium Alloy Forgings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized |
| Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 6Al - 2Sn - 4Zr - 2Mo - 0.08Si Duplex Annealed |
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 2B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
| TABLE 3 | MINIMUM TENSILE PROPERTIES AT 800 °F (427 °C) |
Issuing Committee
AMS G Titanium and Refractory Metals Committee
The committee of Titanium, Beryllium, and Refractory Materials, AMS Committee G, is responsible for preparation, revision, review and approval of documents related to aerospace application of these materials. Included are titanium, beryllium, and refractory metallic such as molybdenum, tantalum, and columbium. The committee provides a forum for interchange of experience and ideas among industry representatives, both suppliers and users, along with interested government agencies, to ensure the utility, proper technical content, and industry acceptance of published documents.