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CONTINENTAL AIRCRAFT ENGINE IO-520 - User Manual

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Publication M-0 CHANGE 4
©
2017 CONTINENTAL MOTORS JUL 2017
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

Magneto RPM Drop Check

Procedure for checking the RPM drop during magneto operation to identify ignition system faults.

Engine Shutdown Procedure

Detailed steps for safely shutting down the engine after testing or operation.

Oil Change Procedure

Steps for performing an engine oil change, including oil sampling and filter inspection.

Engine Operation

Operation After Cylinder Replacement;Overhaul

Guidelines for operating engines after cylinder replacement or major overhaul to ensure proper lubrication and seating.

Non-Overhaul Repair and Replacement

Cylinder Installation

Detailed steps and warnings for installing cylinders, emphasizing proper lubrication and torque.

Cylinder Torque Procedures

Specific procedures and warnings for torquing cylinder fasteners during installation.

Maintenance Standards

CONTINENTAL AIRCRAFT ENGINE IO-520 Specifications

General IconGeneral
Compression Ratio8.5:1
Fuel TypeAvGas 100LL
IgnitionDual Magneto
Cooling SystemAir-cooled
Oil SystemWet sump
Displacement520 cu in
Maximum Power300 hp (224 kW)
Maximum RPM2700
Fuel SystemFuel injection
Redline2700
ConfigurationHorizontally opposed
Bore5.25 inches (133.35 mm)
Stroke4.00 inches (101.6 mm)

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