CONTINENTAL AIRCRAFT ENGINE O-300-C - User Manual

Publication M-0 CHANGE 2
©
2016 CONTINENTAL MOTORS SEP 2016
CONTINENTAL AIRCRAFT ENGINE
MAINTENANCE
MANUAL
STANDARD PRACTICE
FOR SPARK IGNITED ENGINES
Technical Portions Accepted by the Federal Aviation Administration

Summary

Engine Inspection and Service

Engine Time Between Overhaul (TBO)

Lists time between overhaul for various engine models.

6-4.7.1. Fuel System Specifications

Details fuel system specifications and adjustment values for engines.

6-4.7.3. Oil Pump Operational Check

Procedure for checking oil pump operation and pressure.

6-4.7.4. Fuel System Operational Check

Procedure for performing a fuel system operational check.

6-4.7.4.3. Fuel System Operational Checkout Procedure

Step-by-step procedure for the fuel system operational checkout.

Non-Overhaul Repair and Replacement

10-4. Alternator Replacement

Procedure for replacing the alternator.

10-4.1. Gear Driven Alternator Replacement, Forward Mount FWD

Instructions for replacing forward mount gear-driven alternators.

10-4.2. Gear Driven Alternator Replacement, Aft Mount AFT

CONTINENTAL AIRCRAFT ENGINE O-300-C Specifications

General

Number of Cylinders	6
Displacement	301 cu in (4.9 L)
Compression Ratio	7.0:1
Power Output	145 hp (108 kW)
Rated Speed	2700 RPM
Fuel System	Carbureted
Cooling System	Air-cooled
Firing Order	1-4-5-2-3-6
Configuration	Horizontally opposed
Engine Type	Piston
Stroke	3.875 in (98.4 mm)
Fuel Grade	Avgas 80/87
Type	Reciprocating