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Rotax 912 Series Installation Manual

Rotax 912 Series
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d04915.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
INTRO
page 1
August 01/2012
Chapter: INTRO
GENERAL NOTE
Foreword Before starting with the engine installation, read this Installation Manual
carefully. The Manual will provide you with basic information on correct
engine installation, a requirement for safe engine operation.
If any passages of this Manual are not clearly understood or if you have
any questions, please contact an authorized distributor- or Service
Center for ROTAX aircraft engines.
BRP-Powertrain GmbH & Co KG (hereinafter “BRP-Powertrain“) wishes
you much pleasure and satisfaction flying your aircraft powered by this
ROTAX aircraft engine.
Chapter structure The structure of the Manual follows whenever it is possible the structure
of the ATA (Air Transport Association) standards. The aim is the compat-
ibility with the aircraft manufacturer‘s documentation, which means they
must then adapt the documentation to their standard.
The Installation Manual is subdivided into the following chapters:
Subject Chapter
Introduction
Chapter INTRO
List of effective pages
Chapter LEP
Table of amendments
Chapter TOA
General note
Chapter 00-00-00
Storage and Installation
Chapter 10-10-00
Electric system
Chapter 24-00-00
Propeller drive
Chapter 61-00-00
Engine
Chapter 72-00-00
Fuel system
Chapter 73-00-00
Cooling system
Chapter 75-00-00
Engine management
Chapter 76-00-00
Exhaust system
Chapter 78-00-00
Lubrication system
Chapter 79-00-00
Electric starter
Chapter 80-00-00

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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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