Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 25Cr - 20Ni (310S) Solution Heat Treated
- Aerospace Material Specification
- AMS5521K
- Stabilized
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Steel, Corrosion- and Heat-Resistant, Sheet and Strip 16.5Cr - 4.5Ni - 2.9Mo - 0.10N 1850 to 1975 °F (1010 to 1079 °C), Annealed |
| Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 60.5Ni - 23Cr - 14Fe - 0.35Ti - 1.4Al Solution Heat Treated |
| Aerospace Material Specification | Cobalt Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 40Co - 22Cr - 22Ni - 14.5W - 0.07La Solution Heat Treated |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2A | TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 2B | TENSILE PROPERTIES, SI UNITS | |
| TABLE 3 | BENDING PARAMETERS |
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.