Steel, Maraging, Sheet, Strip, and Plate 18Ni - 7.8Co - 4.9Mo - 0.40Ti - 0.10Al Consumable Electrode Melted, Solution Heat Treated
- Aerospace Material Specification
- AMS6520D
- Reaf. Nonc.
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Powder, Chromium Carbide Plus Nickel-Chromium Alloy 75Cr3C2 + 25 (80Ni - 20Cr Alloy) |
| Aerospace Material Specification | Steel Bars and Forgings, Corrosion and Moderate Heat-Resistant 15Cr - 7.1Ni - 2.5Mo - 1.1Al |
| Aerospace Material Specification | Steel, Welding Wire 0.50Cr - 0.55Ni - 0.20Mo (0.18 - 0.23C) (SAE 8620) Vacuum Melted, Environment Controlled Packaging |
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 4A | Minimum Room Temperature Tensile Requirements, Inch/Pound Units | |
| TABLE 4B | Minimum Room Temperature Tensile Requirements, SI Units |
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.