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CONTINENTAL AIRCRAFT ENGINE L/TSIO-360-KB - 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

Engine Inspection and Service

Fuel Injection System Specifications

Provides specifications for fuel injection systems for various engines.

Oil Pump Operational Check

Procedure for checking engine oil pump operation and pressure.

Fuel System Operational Check

Procedure for performing operational checks on the fuel system.

Unscheduled Maintenance

Covers unscheduled maintenance procedures, including propeller strikes.

Troubleshooting

Charging System

Troubleshooting steps for the aircraft charging system.

Starting System

Troubleshooting steps for engine starting system issues.

Non-Overhaul Repair and Replacement

Alternator Replacement

General procedures for replacing engine alternators.

Gear Driven Alternator Replacement, Forward Mount

Procedures for replacing forward-mounted gear-driven alternators.

Gear Driven Alternator Replacement, Aft Mount

Procedures for replacing aft-mounted gear-driven alternators.

CONTINENTAL AIRCRAFT ENGINE L/TSIO-360-KB Specifications

General IconGeneral
Number of Cylinders6
Compression Ratio7.5:1
Fuel Type100LL Aviation Gasoline
Cooling SystemAir-cooled
Fuel SystemFuel injection
Ignition SystemDual Magneto
Oil SystemWet Sump
AspirationTurbocharged
TypeHorizontally opposed
Displacement360 cubic inches (5.9 liters)
Stroke3.875 inches
Power Output210 hp

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