Titanium Alloy, Sheet, Strip, and Plate 6Al - 6V - 2Sn Annealed
- Aerospace Material Specification
- AMS4918K
- Revised
Scope
Recommended Content
Aerospace Material Specification | Titanium Alloy, Hot Rolled Sheet and Strip 5Al - 1Fe Annealed |
Aerospace Material Specification | Titanium Alloy Bars, Forgings, and Forging Stock 4Al - 2.5V - 1.5 Fe Single Hearth Melted, Annealed |
Aerospace Material Specification | Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | Composition | |
TABLE 2A | Tensile Properties, Inch/Pound Units | |
TABLE 2B | Tensile Properties, SI Units | |
TABLE 3 | Bending Requirements |
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.