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Rotax 912 Series Installation Manual

Rotax 912 Series
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d04922.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
72-00-00
page 1
August 01/2012
Chapter: 72-00-00
ENGINE
Introduction
Table of contents This section of the Installation Manual contains views of the aircraft
engine, technical data and installation dimensions of the engine.
WARNUNG
NOTICE
Certification in accordance with the latest regulations,
such as FAR or EASA, must be carried out by the air-
craft or fuselage manufacturer.
Subject Page
Engine components, engine views, cylinder designation
Side view
Front view
Top view
Page 3
Page 3
Page 4
Page 5
Technical data
Weight
Installation dimensions
Centre of gravity of engine and standard accesso-
ries
Moments of inertia
Page 7
Page 7
Page 8
Page 8
Page 8
Operating limits
Deviation from the apparent perpendicular
Page 9
Page 9

Table of Contents

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Rotax 912 Series Specifications

General IconGeneral
Redline5800 rpm
TBO2000 hours
Displacement1211 cc
Bore79.5 mm
Stroke61 mm
Power Output80 hp (59.6 kW)
Compression Ratio9.0:1
Fuel TypeAvgas 100LL
Ignition SystemDual electronic ignition
Fuel SystemFuel Injected
Oil SystemDry sump
Engine Type4-cylinder, horizontally opposed, 4-stroke

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