Chrome Moly 4130 Plate
Hot rolled normalized or annealed 4130 Plate is made from quality steel melted to meet the rigid standards of the aircraft industry. It is carefully rolled and inspected to be free from laminations and tears. It is also free from pits, blisters, grooves, and seams which cannot be removed without reducing tits thickness below the minimum permissible dimensional tolerance limits.
- American Specifications:
- MIL-S-18729, AMS 6350, AMS 6345
- British Specifications:
- 708 A 25
- Applications:
- Intended for general use where welding and moderate tensile properties are required.
- Size Range:
- 3/16" - 6" (5mm - 152 mm)
- Machinability:
- In the annealed condition, 4130 has a machinability rating of 72% based on 1212 as 100%.
- Average Cutting Speed:
- 120 ft/min
- Weldability:
- 4130 may be welded by any of the common welding processes. Preheating and postheating are recommended for difficult weldments.
- Heat Treating:
- Normalize: 1600°F - 1700°F
Quench: oil
Austenitize: 1500°F - 1600°F
Temper: 700°F - 1250°F
| Typical Mechanical Properties | ||
|---|---|---|
| Annealed | Normalized | |
| Tensile Strength (ksi) | 85 max | 90-95 min |
| Yield Point (ksi) | - | 70-75 |
| Elongation (% in 2") | - | 8-18 |
| Typical Chemical Analysis | |
|---|---|
| C | .28 - .33 |
| Mn | .40 - .60 |
| P | .025 max |
| S | .025 max |
| Si | .20 - .35 |
| Cr | .80 - 1.10 |
| Mo | .15 - .25 |
Please note, this information is to be used as a guide only, for more specific information please
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