Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 59Ni - 22Cr - 2.0Mo - 14W - 0.35Al
- Aerospace Material Specification
- AMS5839C
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 47.5Ni - 22Cr - 1.5Co - 9.0Mo - 0.60W - 18Fe |
Aerospace Standard | Quality Management Systems - Requirements for Aviation, Space, and Defense Organizations |
Aerospace Material Specification | Silver Alloy, Brazing Filler Metal 85Ag - 15Mn 1760 to 1780 °F (960 to 971 °C) Solidus-Liquidus Range |
Data Sets - Support Documents
Title | Description | Download |
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[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 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.