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CONTINENTAL AIRCRAFT ENGINE GTSIO-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

Chapter 1. Introduction

1-1.2. Advisories

Explains the types of advisories (WARNING, CAUTION, NOTE) used in the manual for safety.

Engine Inspection and Service

6-4.7.5. Magneto RPM Drop Check

Details the procedure for checking magneto performance by monitoring RPM drop for diagnostics.

6-4.8.2. Oil Change

Provides step-by-step instructions for performing an engine oil change, including sample collection.

Engine Operation

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

Outlines procedures for operating engines after cylinder replacement or major overhaul for proper break-in.

Non-Overhaul Repair and Replacement

10-6.1.1. Cylinder Installation

Details the process for installing cylinders on the engine, including critical pre-installation steps.

10-6.1.3. Cylinder Torque

Specifies the torque sequence and values for cylinder installation to ensure proper seating and seal.

Torque Specifications

Table B-2. Component Specific Torque Specifications

Lists torque specifications for various engine components to ensure correct assembly and safety.

Maintenance Standards

CONTINENTAL AIRCRAFT ENGINE GTSIO-520 Specifications

General IconGeneral
ConfigurationHorizontally Opposed
Compression Ratio7.5:1
Fuel TypeAvgas 100LL
Cooling SystemAir-cooled
Ignition SystemDual magneto
Displacement520 cubic inches
Stroke4.00 inches (101.6 mm)
Horsepower375 hp
Power Output280 kW
Bore5.25 inches (133.35 mm)
Fuel SystemFuel Injected

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