Nickel Alloy, Brazing Filler Metal 92Ni - 4.5Si - 3.1B 1800 to 1900 °F Solidus-Liquidus Range
- Aerospace Material Specification
- AMS4778K
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Nickel Alloy, Brazing Filler Metal 73Ni - 0.75C - 4.5Si - 14Cr - 3.1B - 4.5Fe 1790 °F (977 °C) Solidus to 1970 °F (1077 °C) Liquidus |
| Aerospace Material Specification | Cobalt Alloy, Corrosion and Heat Resistant, Hardfacing Rod and Wire 62Co - 27Cr - 2.9Ni - 5.5Mo |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | STANDARD DIAMETER SIZES | |
| TABLE 3A | DIAMETER TOLERANCES, INCH/POUND UNITS | |
| TABLE 3B | DIAMETER TOLERANCES, SI UNITS | |
| TABLE 4 | STANDARD THICKNESSES | |
| TABLE 5A | PARTICLE SIZE DISTRIBUTION | |
| TABLE 5B | PARTICLE SIZE DISTRIBUTION (METRIC) | |
| Unnamed Dataset 10 |
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.