Forgings, Titanium Alloys Heat-Treated, Finished-Part Properties: Short-Traverse Tensile, Fracture Toughness, and Longitudinal Time-Dependent-Tension
- Aerospace Material Specification
- AMS4938A
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable, Modified Strength |
| Aerospace Material Specification | Forgings, Aluminum Alloys 2xxx and 7xxx, Heat-Treated, Finished-Part Properties: Short-Transverse Tensile Properties and Fracture Toughness |
| Aerospace Material Specification | Electrolytic Treatment for Magnesium Alloys Alkaline Type, Full Coat |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | FLASH EXTENSION TOLERANCES | |
| TABLE 2 | ACCEPTANCE TESTS | |
| TABLE 3 | PERIODIC TESTS | |
| TABLE 4 | ACCEPTANCE SAMPLING PLAN FOR SURFACE CONTAMINATION | |
| Unnamed Dataset 7 |
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.