Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed
- Aerospace Material Specification
- AMS4910N
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| Aerospace Material Specification | Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn, Extra Low Interstitial Annealed |
| Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 13.5V - 11Cr - 3.0Al Solution Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 2B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
| TABLE 3 | BEND FACTOR | |
| TABLE 4 | CRACK DEPTH |
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.