Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 72Ni – 15.5Cr – 1.0Cb(Nb) – 2.4Ti – 0.70Al – 7.0Fe
- Aerospace Material Specification
- AMS5778J
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Manganese Alloy, Brazing Filler Metal 66Mn - 16Ni - 16Co - 0.80B 1770 to 1875 °F (966 to 1024 °C) Solidus-Liquidus Range |
| Aerospace Material Specification | Nickel Alloy, Brazing Filler Metal 92Ni - 4.5Si - 3.1B 1800 to 1900 °F Solidus-Liquidus Range |
| Aerospace Material Specification | Steel, Corrosion-Resistant, Sheet Laminated, Edge Bonded |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1A | Sizes and diameter tolerances, inch/pound units | |
| Table 1B | Sizes and diameter tolerances, SI units |
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.