Titanium Alloy, Hydraulic, Seamless Tubing 3.0a1 2.5v Annealed
- Aerospace Material Specification
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 (316 degrees C) and weldability, but usage is not limited to such applications.
|Aerospace Material Specification||Titanium Alloy, Sheet 6Al - 2Sn - 2Zr - 2Mo - 2Cr - 0.15Si Annealed|
|Aerospace Material Specification||Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated|
|Aerospace Material Specification||Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated and Aged|
Data Sets - Support Documents
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.
|AMS2244||Tolerances, Titanium and Titanium Alloy Tubing|
|AMS2249||Chemical Check Analysis Limits, Titanium and Titanium Alloys|
|AMS2634||ULTRASONIC INSPECTION Thin Wall Metal Tubing|
|AMS2809||Identification Titanium and Titanium Alloy Wrought Products|
|ANSI/ASMEB46.1||This document is not part of the subscrption.|
|ASTME120||This document is not part of the subscrption.|
|ASTME1409||This document is not part of the subscrption.|
|ASTME1447||This document is not part of the subscrption.|
|ASTME8||This document is not part of the subscrption.|