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CONTINENTAL AIRCRAFT ENGINE C85 Series - 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

Manual Introduction and Overview

Supersedure Notice

Notice regarding supersedure of previous service documents.

List of Effective Pages

List of effective pages for the manual and its changes.

Service Documents Incorporated in this Manual

Lists service documents incorporated into the manual.

Engine Inspection and Service

Engine Time Between Overhaul (TBO)

Table listing TBO hours for various engine models.

Fuel System Specifications

Specifications for fuel system adjustment values and pressures.

Oil Pump Operational Check

Procedure for checking oil pump operation and oil pressure.

Alternator Inspection

Procedure for inspecting the alternator during 500-hour service.

Propeller Strike Inspection

Inspecting engine components after a propeller strike.

Troubleshooting Procedures

Fuel Injector Operational Check

Troubleshooting steps for fuel injector system issues.

Charging System Troubleshooting

Troubleshooting procedures for charging system faults.

Starting System Troubleshooting

Troubleshooting steps for engine starting system problems.

Non-Overhaul Repair and Replacement

Alternator Replacement

Procedure for replacing a faulty alternator.

Gear Driven Alternator Removal, Aft Mount

Procedure for removing aft mount gear-driven alternators.

CONTINENTAL AIRCRAFT ENGINE C85 Series Specifications

General IconGeneral
Type4-cylinder, horizontally opposed, air-cooled
Horsepower85 hp
Compression Ratio6.3:1
Weight170 lb (77 kg)
Fuel80/87 octane
Fuel SystemCarbureted
Oil SystemWet sump
Ignition SystemDual Magneto
Stroke3.625 inches
Fuel TypeAvgas
Power Output85 hp at 2575 rpm
Bore3.875 inches (98.4 mm)

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