Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated
- Aerospace Material Specification
- AMS4903
- Issued
Scope
Recommended Content
| 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 and Aged |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | - Composition | |
| TABLE 2A | - Tensile Properties, Inch/Pound Units (See ) | |
| TABLE 2B | - Tensile Properties, Inch/Pound Units (See ) | |
| TABLE 3 | - Bend Factor | |
| TABLE 4A | - Minimum Tensile Properties, Inch/Pound Units (See ) | |
| TABLE 4B | - Minimum Tensile Properties, SI Units (See ) |
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.