Titanium Alloy Tubing, Seamless, Hydraulic 3.0al 2.5v Cold Worked, Stress Relieved
- Aerospace Material Specification
- AMS4944F
- Revised
Scope
This specification covers a titanium alloy in the form of seamless tubing.
This tubing has been used typically for parts, such as hydraulic lines, requiring strength and oxidation resistance up to 600 degrees F (315 degrees C) and weldability, but usage is not limited to such applications.
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Aerospace Material Specification | Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved |
Data Sets - Support Documents
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.