Steel Sheet, Strip, and Plate 1.05Cr - 0.55Ni - 1.0Mo - 0.12V (0.42 - 0.48C) (D6AC) Consumable Electrode Vacuum Melted, Annealed
- Aerospace Material Specification
- AMS6439C
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Hydrogen Embrittlement Relief (Baking) of Steel Parts |
| Aerospace Material Specification | Steel, Bars, Forgings, and Tubing 1.45Cr (0.93-1.05C) (SAE 52100) Special Aircraft-Quality Cleanliness |
| Aerospace Material Specification | Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | MACROSTRUCTURE LIMITS | |
| TABLE 3A | MAXIMUM DECARBURIZATION, INCH/POUND UNITS | |
| TABLE 3B | MAXIMUM DECARBURIZATION, SI UNITS | |
| TABLE 4A | MINIMUM TENSILE PROPERTIES - INCH/POUND UNITS | |
| TABLE 4B | MINIMUM TENSILE PROPERTIES - 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.