Titanium Alloy Sheet 6Al - 4V Driver Sheet
- Aerospace Material Specification
- AMS4932A
- Revised
Scope
Recommended Content
| Aerospace Material Specification | Sampling and Testing of Wrought Titanium Raw Material Except Forgings and Forging Stock |
| Aerospace Material Specification | Titanium Alloy, Forgings 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength |
| Aerospace Material Specification | Titanium Alloy, Forgings 10V - 2Fe - 3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Aged 180 ksi (1241 MPa) Tensile Strength |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| TABLE 1 | Composition | |
| TABLE 2 | Minimum Tensile Properties |
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.
Reference
| Number | Title |
|---|---|
| AMS2249 | CHEMICAL CHECK ANALYSIS LIMITS Titanium and Titanium Alloys |
| 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. |