Steel Sheet, Strip, and Plate, Low Alloy, Heat-Resistant 0.65Si - 1.25Cr - 0.50Mo - 0.25V (0.27 - 0.33C)
- Aerospace Material Specification
- AMS6385L
- Revised
Scope
Rationale
Recommended Content
Aerospace Material Specification | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, Rings, and Forging or Ring Stock 54Ni - 22Cr - 12.5Co - 9.0Mo - 1.2Al Consumable Electrode or Vacuum Induction Melted Annealed |
Aerospace Material Specification | Steel, Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Spheroidized |
Aerospace Material Specification | Nickel-Copper Alloy, Corrosion-Resistant, Sheet, Strip, and Plate 67Ni - 30Cu Annealed |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Table 1 | Composition | |
Table 2 | Macrostructure | |
Table 3A | Maximum total depth of decarburization, inch/pound units | |
Table 3B | Maximum total depth of decarburization, SI units | |
Table 4 | Bend angle | |
Table 5 | Minimum tensile properties at room temperature | |
Table 6 | Minimum 1000 °F (538 °C) 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.