Need help?Do you have a question about the CONTINENTAL AIRCRAFT ENGINE O-200 and is the answer not in the manual?
Outlines the manual's scope, applicable engines, and content of each chapter.
Details supplemental information for ongoing airworthiness for applicable engines.
Defines and explains the use of WARNING, CAUTION, and NOTE advisories.
Explains symbols used to denote variations in engine configuration applicability.
Provides guidance on interpreting manual content, illustrations, and aftermarket parts.
Lists service documents incorporated into the manual and their affected chapters.
Step-by-step guide to performing a magneto RPM drop check on the engine.
Details the steps for safely shutting down the engine after testing.
Step-by-step instructions for performing an engine oil change and filter inspection.
Step-by-step guide for installing cylinders, including lubrication and torque.
Details the torque sequence and values for cylinder installation.
Step-by-step guide for installing a solid nose oil seal.
Procedures for removing a split nose oil seal.
Step-by-step guide for installing a split type nose oil seal.
Lists specific torque values for various fasteners and components.
Lists parts that must be replaced during engine overhaul based on condition or 100% replacement.
Provides instructions and warnings for applying Gasket Maker sealant.
Details steps for installing gaskets, including sealant use and torque.
Explains the use and installation of crush washers for sealing.
General| Number of Cylinders | 4 |
|---|---|
| Compression Ratio | 7.0:1 |
| Fuel Type | Aviation gasoline |
| Oil System | Wet sump |
| Type | Horizontally opposed, four-cylinder |
| Displacement | 201 cu in (3.29 L) |
| Stroke | 3.875 in (98.4 mm) |
| Max Power | 100 hp (75 kW) at 2750 rpm |
| Fuel Grade | 80/87 |
| Fuel System | Float type carburetor |
| Dry Weight | 170 lbs (77 kg) |
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