Steel, Corrosion-Resistant, Bars, and Forgings 10Cr - 5.5Ni - 14Co - 2Mo - 1W (0.19-0.23C) Vacuum Induction Melted, Vacuum Arc Remelted, Normalized, Annealed
- Aerospace Material Specification
- AMS5922C
- Revised
Scope
Rationale
Recommended Content
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| Aerospace Material Specification | Heat Treatment of Steel Raw Materials |
| Aerospace Material Specification | Titanium Alloy, Forgings 10V - 2Fe - 3Al Consumable Electrode Melted, Single-Step Solution Heat Treated and Aged 180 ksi (1241 MPa) Tensile Strength |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Composition | |
| Table 2 | Macrostructure limits | |
| Table 3 | Micro-inclusion rating limits | |
| Table 4 | Minimum tensile properties |
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.