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CONTINENTAL AIRCRAFT ENGINE A65 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

Service Documents Incorporated

Service Documents Incorporated in Manual

Lists service documents incorporated into the manual.

Fuel Injection System Specifications

Fuel System Adjustment Values

Table of idle and full power fuel pressures and flows for engines.

Oil Pump Operational Check

Fuel System Operational Check

Fuel System Operational Checkout Setup Instructions

Instructions for setting up test equipment for fuel system checkout.

Fuel System Operational Checkout Procedure

Step-by-step procedure for performing a fuel system operational checkout.

Alternator Inspection

Alternator Drive Hub Inspection

Procedure for inspecting the alternator drive hub.

Unscheduled Maintenance

Propeller Strike Inspection

Inspection procedures following a propeller strike incident.

Charging System Troubleshooting

Starting System Troubleshooting

Alternator Replacement

Gear Driven Alternator Removal (Forward Mount)

Procedure for removing a forward mount gear-driven alternator.

Alternator Drive Hub Removal (Forward Mount)

Procedure for removing the alternator drive hub assembly.

Alternator Drive Hub Installation (Forward Mount)

Procedure for installing the alternator drive hub assembly.

Gear Driven Alternator Installation (Forward Mount)

Procedure for installing a forward mount gear-driven alternator.

Gear Driven Alternator Replacement (Aft Mount)

Gear Driven Alternator Removal (Aft Mount)

Procedure for removing an aft mount gear-driven alternator.

Alternator Drive Hub Removal (Aft Mount)

Procedure for removing the alternator drive hub assembly (aft mount).

Alternator Drive Hub Installation (Aft Mount)

Procedure for installing alternator drive hub assembly (aft mount).

Gear Driven Alternator Installation (Aft Mount)

Procedure for installing an aft mount gear-driven alternator.

CONTINENTAL AIRCRAFT ENGINE A65 Series Specifications

General IconGeneral
Type4-cylinder, horizontally opposed, air-cooled
Compression Ratio6.3:1
Fuel SystemCarbureted
Oil SystemWet sump
Ignition SystemDual magneto
Displacement171 cu in (2.8 L)
Horsepower65 hp
Bore3.875 inches
Stroke3.625 inches
Weight170 lbs (77 kg)
RPM at Max Power2, 300 rpm
Fuel TypeAvgas 80/87

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