Do you have a question about the CONTINENTAL AIRCRAFT ENGINE IO-520 and is the answer not in the manual?
Procedure for checking the RPM drop during magneto operation to identify ignition system faults.
Detailed steps for safely shutting down the engine after testing or operation.
Steps for performing an engine oil change, including oil sampling and filter inspection.
Guidelines for operating engines after cylinder replacement or major overhaul to ensure proper lubrication and seating.
Detailed steps and warnings for installing cylinders, emphasizing proper lubrication and torque.
Specific procedures and warnings for torquing cylinder fasteners during installation.
| Compression Ratio | 8.5:1 |
|---|---|
| Fuel Type | AvGas 100LL |
| Ignition | Dual Magneto |
| Cooling System | Air-cooled |
| Oil System | Wet sump |
| Displacement | 520 cu in |
| Maximum Power | 300 hp (224 kW) |
| Maximum RPM | 2700 |
| Fuel System | Fuel injection |
| Redline | 2700 |
| Configuration | Horizontally opposed |
| Bore | 5.25 inches (133.35 mm) |
| Stroke | 4.00 inches (101.6 mm) |