NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND FOIL 52.5Ni - 19Cr - 3.0Mo - 5.0Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted Precision Cold Rolled, Solution Heat Treated
- Aerospace Material Specification
- MAM5914
- Issued
Scope
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2 | Maximum Surface Roughness | |
| TABLE 3 | Tensile Properties | |
| TABLE 4 | Maximum Average Grain Size | |
| TABLE 5 | Maximum Inclusion or Stringer Size | |
| TABLE 6 | Minimum Room Temperature Tensile Properties | |
| TABLE 7 | Minimum 650 °C Tensile Properties | |
| TABLE 8 | Width Tolerance |
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.