Do you have a question about the CONTINENTAL AIRCRAFT ENGINE L/TSIO-360-KB and is the answer not in the manual?
Provides specifications for fuel injection systems for various engines.
Procedure for checking engine oil pump operation and pressure.
Procedure for performing operational checks on the fuel system.
Covers unscheduled maintenance procedures, including propeller strikes.
Troubleshooting steps for the aircraft charging system.
Troubleshooting steps for engine starting system issues.
General procedures for replacing engine alternators.
Procedures for replacing forward-mounted gear-driven alternators.
Procedures for replacing aft-mounted gear-driven alternators.
| Number of Cylinders | 6 |
|---|---|
| Compression Ratio | 7.5:1 |
| Fuel Type | 100LL Aviation Gasoline |
| Cooling System | Air-cooled |
| Fuel System | Fuel injection |
| Ignition System | Dual Magneto |
| Oil System | Wet Sump |
| Aspiration | Turbocharged |
| Type | Horizontally opposed |
| Displacement | 360 cubic inches (5.9 liters) |
| Stroke | 3.875 inches |
| Power Output | 210 hp |