Rotax 912 Series Operator's Manual

CGSB Canadian General Standards Board
DCDI Dual Capacitor Discharge Ignition
DC direct current
DOA Design Organisation Approval
DOT Department of Transport
EASA European Aviation Safety Agency
IM Installation Manual
ECU Engine Control Unit
EGT Exhaust Gas Temperature
INTRO Introduction
EMS Engine Management System
EN European Norm
ETFE Ethylene Tetrafluoroethylene
FAA Federal Aviation Administration
FAR Federal Aviation Regulations
hr. hours
HIC A Harness Interface Connector A
HIC B Harness Interface Connector B
IFR Instrument Flight Rules
INJ 1–8 Injector 1–8
IPC Illustrated Parts Catalog
ips inch per second
iRMT independent ROTAX Maintenance Technician
TOC Table of content
ISA International Standard Atmosphere
kg Kilograms
KNOCK Knock sensor
MAPS 1+2 Manifold Air Pressure Sensor 1+2
MATS 1+2 Manifold Air Temperature Sensor 1+2
MS Magneto Side
MON Motor Octane Number
Page 1-4
November 01/2016
BRP-Rotax Effectivity: 912 Serie
Edition 4 / Rev. 0

Rotax 912 Series Specifications

General

Redline	5800 rpm
TBO	2000 hours
Displacement	1211 cc
Bore	79.5 mm
Stroke	61 mm
Power Output	80 hp (59.6 kW)
Compression Ratio	9.0:1
Fuel Type	Avgas 100LL
Ignition System	Dual electronic ignition
Fuel System	Fuel Injected
Oil System	Dry sump
Engine Type	4-cylinder, horizontally opposed, 4-stroke