Steel, Welding Wire 0.06 Carbon, Maximum
- Aerospace Material Specification
- AMS5030K
- Stabilized
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Nickel-Iron Alloy, Corrosion and Heat-Resistant, Welding Wire 12.5Cr - 42.5Ni - 6.0Mo - 2.7Ti - 0.015B - 35Fe |
| Aerospace Material Specification | Titanium Alloy Bars, Wire, and Rings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized |
| Aerospace Material Specification | Steel, Corrosion- and Heat-Resistant, Welding Wire 27Cr - 21.5Ni |
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Sizes and Diameter Tolerances, Inch/Pound Units | |
| TABLE 2B | Sizes and Diameter Tolerances, SI Units |
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.