Steel, Corrosion-Resistant, Bars, Wire, and Forgings 12Cr - 11Ni - 1.7Ti - 1Mo Vacuum Induction Plus Vacuum Consumable Electrode Remelted Solution Heat Treated, Precipitation Hardenable
- Aerospace Material Specification
- AMS5936C
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Steel, Corrosion and Heat-Resistant, Bars, Wire, and Forgings 12.5Cr - Low Carbon (SAE 51416, 51416Se) Free-Machining |
| Aerospace Material Specification | Steel, Corrosion-Resistant, Bars, Wire, and Forgings 17Cr - 0.52Mo (0.95 - 1.20C) (440C) |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | MACROSTRUCTURE LIMITS | |
| TABLE 3 | PRECIPITATION HEAT TREATING PARAMETERS | |
| TABLE 4A | MINIMUM TENSILE PROPERTIES, INCH/POUND UNITS | |
| TABLE 4B | MINIMUM TENSILE PROPERTIES, SI UNITS | |
| TABLE 5 | MINIMUM HARDNESS | |
| TABLE 6 | MINIMUM FRACTURE TOUGHNESS, K |
Issuing Committee
AMS F Corrosion and Heat Resistant Alloys Committee
The committee of Corrosion and Heat Resistant Steels and Alloys and Specialty Steels and Alloys, AMS Committee F, will prepare, coordinate, and revise documents related to corrosion and heat resistant steels and alloys and specialty steels and alloys technology, such as stainless steels and nickel and base alloys, 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.