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Explains variations between C125, C145, and O-300 engine models.
Provides physical and performance specifications for engine models.
Lists engine accessories, manufacturers, and part numbers.
Explains variations between C125, C145, and O-300 engine models.
Details the engine's lubricating system and oil flow.
Steps for removing the engine from the aircraft.
Pre-flight checks and procedures before starting the engine.
Steps for starting the aircraft engine.
Procedures for warming up and testing the engine on the ground.
Troubleshooting steps for engine starting failures.
Diagnosis and repair for low oil pressure issues.
Routine daily checks for the engine.
Procedures for the 100-hour engine inspection.
Instructions for carburetor adjustment and maintenance.
Steps for installing and timing magnetos.
Steps for reassembling major engine components.
Procedures for final engine assembly.
Specifies limits for crankcase dimensions and fits.
Specifies limits for crankshaft dimensions and fits.
Installation, operation, and maintenance for the Marvel-Schebler MA-3SPA carburetor.
Classifies common types of hydraulic tappet failures.
General| Number of Cylinders | 6 |
|---|---|
| Compression Ratio | 7.0:1 |
| Maximum RPM | 2700 |
| Cooling System | Air-cooled |
| Maximum Power | 145 hp (108 kW) |
| Fuel Type | AvGas |
| Type | Horizontally Opposed, Air Cooled |
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