Steel, Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Normalized or Otherwise Heat Treated
- Aerospace Material Specification
- AMS6345A
- Revised
Scope
Recommended Content
| Technical Paper | Optimizing Forgings for Automotive Transmission Hubs by Warm Forming Vanadium-Microalloyed Steels |
| Aerospace Material Specification | Wire, Steel 0.18 - 0.23C (SAE 1020) Annealed |
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Composition | |
| TABLE 2A | Minimum Tensile Properties, Inch/Pound Units | |
| TABLE 2B | Minimum Tensile Properties, SI Units | |
| TABLE 3A | Maximum Decarburization, Inch/Pound Units | |
| TABLE 3B | Maximum Decarburization, SI Units | |
| TABLE 4 | Bending Parameters | |
| TABLE 5 | Minimum Hardness, As Quenched |
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.