BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded
- Aerospace Material Specification
|Aerospace Material Specification||BOLTS AND SCREWS, LOW-ALLOY STEEL Heat Treated, Roll Threaded|
|Aerospace Standard||Bolts and Screws, UNS N07001 Tensile Strength 1210 MPa, Thread and Fillet Radius Rolled Before Aging, Procurement Specification, Metric|
Data Sets - Support Documents
|Unnamed Dataset 1|
|TABLE I||AMERICAN NATIONAL & UNIFIED THREADS|
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.