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Lists engine interface requirements not supplied with the engine by CM.
Describes internal components like the crankcase, drive train, and cylinders.
Presents technical specifications for O-200-D and O-200-X engines.
Covers common tools, receipt, handling, and inspection for installation.
Details steps for preparing the aircraft and engine for installation.
Lists essential checks and procedures to be completed before flight.
Supplements AFM/POH procedures for normal engine operation.
Supplements AFM/POH for emergency procedures and conditions.
General| Compression Ratio | 7.0:1 |
|---|---|
| Fuel System | Carburetor |
| Fuel Type | Avgas 100LL |
| Oil System | Wet Sump |
| Displacement | 201 cubic inches |
| Horsepower | 100 hp (75 kW) |
| Bore | 4.06 inches (103 mm) |
| Stroke | 3.875 in (98.4 mm) |
| Maximum RPM | 2750 |
| Dry Weight | 170 lbs (77 kg) |
| Type | 4-cylinder, horizontally opposed, air-cooled |
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