TITANIUM ALLOY, SEAMLESS, HYDRAULIC TUBING 15V - 3.0Cr - 3.0Al - 3.0Sn Cold Worked and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4922A
- Revised
Scope
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Hydraulic, Seamless Tubing 3.0Al - 2.5V Annealed |
| Aerospace Material Specification | Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved |
| Aerospace Material Specification | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1 | Composition | |
| TABLE 2 | Minimum Tensile Properties | |
| TABLE 3 | Flattening Test | |
| TABLE 4A | Outer Diameter, Tolerances, Inch/Pound Units | |
| TABLE 4B | Outer Diameter, Tolerances, SI Units |
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.