Steel, Corrosion Resistant, Sheet and Strip 17Cr – 7.1Ni – 1.1Al Solution Heat Treated and Cold Rolled, Precipitation Hardenable 0.0015 to 0.050 Inch (0.038 to 1.27 mm) Nominal Thickness
- Aerospace Material Specification
- AMS5529H
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Steel, Corrosion and Heat-Resistant, Sheet, Strip, Foil, and Plate 15Cr - 7.1Ni - 2.5Mo - 1.1Al Solution Heat Treated, Precipitation Hardenable |
| Aerospace Material Specification | Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 25Cr - 20Ni (310S) Solution Heat Treated |
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 AS PRECIPITATION HEAT TREATED TO CH900 CONDITION |
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.