Rotax 912 ULS 3 Operator's Manual page 63

Introduction
Table of content
Effectivity: 912 Serie
OM Edition 2 / 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
Coolant
Expansions tank
Coolant temperature measuring
Fuel system
Fuel
Return line
Lubrication system
Lubrication
Crankcase
Oil pump
Oil circuit vented
Oil temperature sensor
Electric system
Charging coils
Propeller gearbox
Reduction ratio
Overload clutch
Torsional shock absorber
Backlash
Vacuum pump
BRP-Powertrain
Page
page 7-2
page 7-2
page 7-2
page 7-2
page 7-4
page 7-4
page 7-4
page 7-5
page 7-5
page 7-5
page 7-5
page 7-5
page 7-5
page 7-7
page 7-7
page 7-8
page 7-8
page 7-8
page 7-8
page 7-9
page 7-9
page 7-1
April 01/2010