NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, FOIL, AND PLATE 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated
- Aerospace Material Specification
- AMS5596H
- Revised
Scope
Recommended Content
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 | Maximum Hardness | |
| TABLE 4 | Bending Parameters | |
| TABLE 5A | Minimum Room Temperature Tensile Properties, Inch/Pound Units | |
| TABLE 5B | Minimum Room Temperature Tensile Properties, SI Units | |
| TABLE 6A | Minimum Elevated Temperature Tensile Properties, Inch/Pound Units | |
| TABLE 6B | Minimum Elevated Temperature Tensile Properties, SI Units | |
| TABLE 7A | Stress-Rupture Properties, Inch/Pound Units | |
| TABLE 7B | Stress-Rupture Properties, 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.