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Rotax 912 i series Installation Manual

Rotax 912 i series
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d05165.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 0
10-10-00
Page 1
January 01/2012
Chapter: 10-10-00
STORAGE AND INSTALLATION
Introduction
Table of contents This section of the installation manual contains state of delivery, trans-
port, storage and aircraft engine installation.
WARNUNG
NOTICE
The stated directives are measures that must be ob-
served during every engine installation to prevent any
accidents and engine damage.
Subject Page
Preparations for engine installation
State of delivery
Unpacking/handling of the engine
Preservation and storage of the engine
Protective coverings
Page 3
Page 3
Page 3
Page 4
Page 4
Engine suspension and installation position
Engine suspension instructions
Attachment points
Definition of attachment points
Permissible installation positions
Page 6
Page 6
Page 8
Page 9
Page 11

Table of Contents

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Rotax 912 i series Specifications

General IconGeneral
Number of Cylinders4
Max Power100 hp (73.5 kW)
Max Power Output RPM5800 rpm
Ignition SystemDual electronic ignition
Oil SystemDry sump, forced lubrication with separate oil tank
Reduction Gear Ratio2.43:1
TBO2000 hours
Engine Type4-stroke, horizontally opposed
Displacement1352 cm³
Bore x Stroke84 mm x 61 mm
Max Torque128 Nm
Fuel TypeAvgas 100LL or unleaded automotive gasoline
Fuel SystemElectronic fuel injection
Cooling SystemLiquid/air-cooled

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