Nickel Wire and Ribbon 99Ni
- Aerospace Material Specification
- AMS5555D
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Steel, Corrosion-Resistant, Bars and Wire 18Cr - 9.0Ni (302) Solution Heat Treated and Cold Drawn 100 ksi (689 MPa) Tensile Strength |
| Aerospace Material Specification | Chemical Check Analysis Limits, Corrosion- and Heat-Resistant Steels and Alloys, Maraging and Other Highly Alloyed Steels, and Iron Alloys |
| Aerospace Material Specification | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 19Cr - 10Ni Solution Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Round Wire Tolerances, Inch/Pound Units | |
| TABLE 2B | Round Wire 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.