Need help?Do you have a question about the CONTINENTAL AIRCRAFT ENGINE O-200-A and is the answer not in the manual?
Details specifications for fuel injection system adjustment values.
Steps for inspecting engine after a propeller strike incident.
Diagnostic steps for engine starting system failures.
Procedure for installing forward mount gear driven alternators.
Procedure for installing aft mount gear driven alternators.
General| Type | 4-cylinder, horizontally opposed, air-cooled |
|---|---|
| Compression Ratio | 7.0:1 |
| Fuel System | Carburetor |
| Oil System | Wet sump |
| Displacement | 201 cubic inches (3.29 liters) |
| Bore | 4.06 inches (103.1 mm) |
| Stroke | 3.875 in (98 mm) |
| Maximum Power | 100 hp (75 kW) at 2, 750 rpm |
| Weight | 170 lb (77 kg) |
| Fuel Type | Avgas 80/87 |
| Ignition System | Dual magneto |
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