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CONTINENTAL AIRCRAFT ENGINE IO-360 - 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

Table 6-4. Fuel System Adjustment Values

Provides fuel system adjustment values for various engine models at idle and full power.

6-4.7.5. Magneto RPM Drop Check

Details the procedure for checking magneto RPM drop to diagnose ignition system issues.

6-4.8.2. Oil Change

Describes the process for changing engine oil, including sample collection and filter inspection.

Engine Operation

7-2.3. Engine Operation after Cylinder Replacement and;or Major Overhaul

Details procedures for operating engines after cylinder replacement or major overhaul.

Non-Overhaul Repair and Replacement

10-6.1.2. Cylinder Installation

Provides detailed instructions for installing cylinders on the engine.

10-6.1.3. Cylinder Torque

Details the correct torque values and sequence for cylinder installation.

10-10.2. Solid Nose Oil Seal Installation

Outlines the procedure for installing a solid nose oil seal.

10-10.3. Split Nose Oil Seal Removal

Describes the process for removing split type nose oil seals.

Torque Specifications

CONTINENTAL AIRCRAFT ENGINE IO-360 Specifications

General IconGeneral
Compression Ratio8.5:1
Fuel TypeAvgas 100LL
Oil SystemWet sump
IgnitionDual magneto
TypeHorizontally Opposed, Four-Cylinder
Displacement360 cu in (5.9 L)
Bore5.125 in (130.2 mm)
Stroke4.375 in (111.1 mm)
Fuel SystemFuel Injected

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