Cobalt Alloy, Corrosion- and Heat-Resistant, Hard Facing Rods and Wire 62Co - 29Cr - 4.5W - 1.2C
- Aerospace Material Specification
- AMS5788G
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Welding Wire 8Al - 1Mo - 1V |
| Aerospace Material Specification | Cobalt Alloy, Corrosion and Heat Resistant, Hardfacing Rod and Wire 62Co - 27Cr - 2.9Ni - 5.5Mo |
| Aerospace Material Specification | Nickel Alloy, Brazing Filler Metal 82Ni - 4.5Si - 7.0Cr - 3.1B - 3.0Fe 1780 °F (971 °C) Solidus to 1830 °F (999 °C) Liquidus Range |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Table 1 | Composition | |
| Table 2 | Standard sizes and diameter tolerances |
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, 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.