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Describes the oil flow and components within the engine's lubrication system.
Explains the function and components of the turbocharger system.
Describes the conventional twin ignition system and its operation.
Details the multi-nozzle, continuous-flow fuel injection system.
Lists key technical specifications for the TSIO-520-BE engine.
Details critical operating parameters such as RPM, pressure, and temperatures.
Guidelines for installing the engine into the airframe.
Procedures for engine checks before flight and during run-up.
Step-by-step instructions for starting the engine.
Essential checks to perform before taking off.
Instructions for controlling power and executing takeoff.
Recommendations for engine settings during cruise flight.
Procedure to follow if a fire is observed during engine starting.
Actions to take in case of a turbocharger failure.
Actions for low oil pressure and in-flight engine restarting.
Follow airframe manufacturer's instructions for in-flight engine fires.
Procedure for performing cylinder leakage checks.
Lists common engine troubles, probable causes, and corrections.
Diagnosing and correcting issues with the ignition system.
Diagnosing and correcting issues with the oil system.
Diagnosing and correcting issues with the fuel injection system.
General| Number of Cylinders | 6 |
|---|---|
| Displacement | 520 cu in (8.5 L) |
| Compression Ratio | 7.5:1 |
| Fuel Type | Avgas 100LL |
| Oil System | Wet sump |
| Cooling System | Air-cooled |
| Type | Horizontally Opposed |
| Bore | 5.25 inches (133.35 mm) |
| Stroke | 4.00 in (102 mm) |
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