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Rotax 912 i series Operator's Manual

Rotax 912 i series
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Effectivity: 912 i Series BRP-Powertrain page INTRO-1
OM Edition 1/Rev. 0 January 01/2012
d05270.fm
Introduction
Foreword BRP-Powertrain provides “Instructions of Continued Airworthi-
ness”, which are based on the design, the tests and certification
of the engine and its components. These instructions apply only
to engines and components supplied by BRP-Powertrain.
This Operator Manual contains important information about safe
operation of the engine, together with descriptions of the system
and its layout, technical data, operating media and the operational
limits of the engine.
The specified data apply only to the engine and not to specific ap-
plications in particular aircraft. The aircraft manufacturers Opera-
tors Manual is therefore definitive in terms of the operation of the
engine, as it contains all of the aircraft-specific instructions.
Chapter structure The structure of the Manual follows whenever it is possible the
structure of the „GAMA Specification #1 for Pilot’s Operating
Handbook“. The Operators 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 1)
Operating instructions Chapter 2)
Standard operation Chapter 3)
Abnormal operation Chapter 4)
Performance data Chapter 5)
Weights Chapter 6)
Description of systems Chapter 7)
Checks Chapter 8)
Supplements Chapter 9)

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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