Steel, Bars, and Forgings 3.5Cr - 9.5Ni - 18Co - 1.1Mo (0.13 – 0.17C) Double Vacuum Melted, Normalized, Annealed
- Aerospace Material Specification
- AMS6517
- Issued
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Iron, Commercially Pure, Bar, Sheet, Strip, and Plate Hot Rolled, Unannealed |
| Aerospace Material Specification | Steel Sheet, Strip, and Plate, Low Alloy, Heat-Resistant 0.65Si - 1.25Cr - 0.50Mo - 0.25V (0.27 - 0.33C) |
| Aerospace Material Specification | Steel Strip (0.90 - 1.04C) (SAE 1095) Hard Temper |
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 LONGITUDINAL TENSILE PROPERTIES | |
| TABLE 5 | MINIMUM TRANSVERSE TENSILE PROPERTIES |
Issuing Committee
AMS E Carbon and Low Alloy Steels Committee
The committee of Carbon and Low Alloy Steels, AMS Committee E, shall prepare, coordinate, and revise documents related to carbon and low alloy steels technology, such as steel cleanliness and steel quality assurance sampling, 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.