Steel, Corrosion and Heat Resistant, Flat Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 °F (982 °C) Solution Treated, Cold Drawn or Cold Rolled and Aged, Consumable Electrode Remelted
- Aerospace Material Specification
- AMS5810B
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Wire, Steel Welding 18.5Ni - 8.5Co - 5.2Mo - 0.72Ti - 0.10Al (Marage 300) Vacuum Melted, Environment Controlled Packaging |
| Aerospace Material Specification | Steel, Mechanical Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337) |
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | HARDNESS | |
| TABLE 3A | THICKNESS TOLERANCE, INCH/POUND UNITS | |
| TABLE 3B | THICKNESS TOLERANCE, SI UNITS | |
| TABLE 4A | WIDTH TOLERANCE, INCH/POUND UNITS | |
| TABLE 4B | WIDTH TOLERANCE, SI UNITS |
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.