Titanium, Sheet, Laminated, Surface Bonded
- Aerospace Material Specification
- AMS4949A
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Phosphor Bronze, Sheet, Strip, and Plate 94.5Cu - 4.0Sn - 0.19P Spring Temper (H08) |
Aerospace Material Specification | Steel, Carbon, Laminated Sheet, Surface Bonded |
Aerospace Material Specification | Steel, Sheet and Strip 0.15 Carbon, Maximum Half Hard Temper |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | THICKNESS COMBINATIONS OF SHIM STOCK | |
TABLE 2A | TOTAL THICKNESS TOLERANCES, INCH-POUND UNITS | |
TABLE 2B | TOTAL THICKNESS TOLERANCES, SI UNITS |
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.