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Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed
- Aerospace Material Specification
- AMS4911R
- Revised
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm) inclusive in thickness.
Rationale
AMS4911R adds skull melting as a first melt in remelted applications (3.2 and 4.4.1) and exception notice (3.9).
Recommended Content
| Aerospace Material Specification | Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa) |
| Aerospace Material Specification | Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Annealed |
| Aerospace Material Specification | Titanium and Titanium Alloy, Sheet, Strip, and Plate |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| [Unnamed Dataset 1] | ||
| [Unnamed Dataset 2] | ||
| Table 1 | Composition | |
| Table 2A | Minimum tensile properties, inch/pound units | |
| Table 2B | Minimum tensile properties, SI units | |
| Table 3 | Bending parameters |
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
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