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CONTINENTAL AIRCRAFT ENGINE O-300-A - User Manual

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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
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Summary

Fuel System Specifications

Oil Pump Operational Check

Fuel System Operational Check

Fuel System Operational Checkout Setup Instructions

Fuel System Operational Checkout Procedure

Alternator Inspection

Alternator Drive Hub Inspection FWD

Unscheduled Maintenance

Propeller Strike

Addresses incidents where the propeller contacts a foreign object.

Procedure

Step-by-step guide for inspecting engine components after a propeller strike.

Charging System

Starting System

Alternator Replacement

Alternator Drive Hub Removal FWD

Alternator Drive Hub Installation FWD

Alternator Drive Hub Slippage Inspection FWD

Gear Driven Alternator Installation FWD

Gear Driven Alternator Replacement, Aft Mount AFT

Alternator Drive Hub Removal AFT

Alternator Drive Hub Installation AFT

Gear Driven Alternator Installation AFT

CONTINENTAL AIRCRAFT ENGINE O-300-A Specifications

General IconGeneral
Number of Cylinders6
Horsepower145 hp
Compression Ratio7.0:1
Rated Speed2700 RPM
Fuel SystemCarbureted
Cooling SystemAir-cooled
TypeHorizontally opposed, air-cooled
Displacement300 cu in (4.9 L)
Stroke3.875 in (98.4 mm)
Fuel GradeAvgas 80/87

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