Nickel Alloy, Corrosion and Heat-Resistant, Plate 54Ni - 22Cr - 12.5Co - 9.0Mo - 1.2Al Annealed
- Aerospace Material Specification
- AMS5888C
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 74Ni - 15.5Cr - 8.0Fe Annealed |
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe Annealed |
Aerospace Material Specification | Alloy Sheet, Strip, and Plate, Corrosion and Heat Resistant 80Ni - 15.5Cr - 0.62Ti - 3.25Al Annealed |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | COMPOSITION | |
TABLE 2 | MINIMUM TENSILE PROPERTIES | |
TABLE 3 | MINIMUM TENSILE PROPERTIES | |
TABLE 4 | MINIMUM ELEVATED TEMPERATURE 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.