CONTINENTAL AIRCRAFT ENGINE TSIO520 - User Manual

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

Summary

6-4.7.5. Magneto RPM Drop Check

CAUTION

Caution regarding single ignition and RPM drop.

6-4.7.6. Engine Shutdown

Procedure

Steps for shutting down the engine.

6-4.8.2. Oil Change

Procedure

Steps for performing an oil change.

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

1. Operation After Major Overhaul Utilizing an Engine Test Cell

2. Operation After Major Overhaul Utilizing The Aircraft in Lieu of an Engine Test Cell.

3. Engine Operation After Cylinder Overhaul or New Cylinder Installation

10-6.1.2. Cylinder Installation

10-6.1.3. Cylinder Torque

10-10.2. Solid Nose Oil Seal Installation

10-10.3. Split Nose Oil Seal Removal

10-10.4. Split Type Nose Oil Seal Installation

Table B-2. Component Specific Torque Specifications

C-2.4. Mandatory Overhaul Replacement Parts

Table C-1. Mandatory Overhaul Replacement Parts

Lists parts that must be replaced during overhaul.

C-10. Gasket Installation

WARNING

Warning on sealant use for gasket installation.

C-10.1. Crush Washer Installation

CONTINENTAL AIRCRAFT ENGINE TSIO520 Specifications

General

Number of Cylinders	6
Compression Ratio	7.5:1
Type	Turbocharged, fuel-injected
Displacement	520 cubic inches
Bore	5.25 inches
Stroke	4.00 inches
Fuel Type	Avgas 100LL
Oil Capacity	12 quarts
Weight	467 lbs (212 kg) dry