Steel Tubing, Welded 0.13 Carbon, Maximum Annealed
- Aerospace Material Specification
- AMS5053H
- Reaffirmed
Scope
Recommended Content
| Aerospace Material Specification | Tantalum Alloy Sheet, Strip, and Plate 90Ta - 10W |
| Aerospace Standard | NUT, SELF-LOCKING, CASTELLATED, PREVAILING TORQUE, UNS G41300 OR UNS G43400, UNJ 16 PITCH THREAD FORM |
| Aerospace Material Specification | Chemical Check Analysis Limits Titanium and Titanium Alloys |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2 | Minimum Tensile Properties | |
| TABLE 3 | Minimum OD Increase, Percent |
Issuing Committee
AMS E Carbon and Low Alloy Steels Committee
The committee of Carbon and Low Alloy Steels, AMS Committee E, shall prepare, coordinate, and revise documents related to carbon and low alloy steels technology, such as steel cleanliness and steel quality assurance sampling, through the participation of metals suppliers, users, and interested government agencies. Committee activities shall provide a forum for the cooperative interchange of ideas and experience of the participants, resulting in the publication of specifications that embody sound, established aerospace industry practices and requirements to serve the suppliers and customers of aerospace materials.