Titanium and Titanium Alloy, Bars (Rolled or Forged) and Reforging Stock, Aircraft Quality
- Aerospace Material Specification
- AMST9047
- Issued
Scope
Recommended Content
Aerospace Material Specification | Titanium and Titanium Alloy, Bars (Rolled or Forged) and Reforging Stock, Aircraft Quality |
Aerospace Material Specification | Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated |
Aerospace Material Specification | Titanium Alloy Bars, Wire, and Rings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
TABLE 1 | Chemical composition, percent by weight. & | |
TABLE 2 | Commercially pure and alpha titanium minimum tensile properties. | |
TABLE 3 | Alpha-Beta titanium alloys minimum tensile properties | |
TABLE 4 | Beta titanium alloys minimum tensile properties | |
TABLE 5 | Minimum ultrasonic quality levels | |
TABLE 6 | Forged bar and reforging stock dimensional tolerances | |
TABLE 7 | Bar products quality conformance sampling | |
TABLE 8 | Tension specimen requirements | |
TABLE 9 | Cross-reference composition classification |
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.