Rotax 912 i series Operator's Manual page 67

Introduction
Table of content
Effectivity: 912 i Series
OM Edition 1/Rev. 0
7) Description of systems
This chapter of the Operator Manual contains the description of
cooling system, fuel system, lubrication system, electric system
and the propeller gearbox.
As already mentioned in the preface, the system descriptions only
apply to the engine, not to a specific application in a particular air-
craft. The aircraft manufacturers Operators Manual is therefore
definitive in terms of the operation of the engine, as it contains all
the aircraft specific instructions.
Subject
Cooling system of engine
Cooling
Coolant
Expansions tank
Coolant temperature measuring
Fuel system
Fuel
Fuel pump switches
Fuel pressure regulator
Return line
Lubrication system
Lubrication
Crankcase
Oil pump
Oil venting system
Oil temperature sensor
Oil pressure sensor
Electric system
EMS overview
EMS power supply
LANE select switch A/B
EMS main switch
Ignition system
Fuel injection
ECU
Main functions of the ECU
Propeller gearbox
Reduction ratio
Torsional shock absorber
Governor
BRP-Powertrain
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January 01/2012