BRP-Rotax
INSTALLATION MANUAL
Abbreviations Description
CW
clockwise
CCW
counter-clockwise
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
EMS GND Engine system internal ground reference which is intended to be dis-
connected from aircraft common ground during flight
EMC
Electromagnetic compatibility
EN
European Standard
ETFE
Ethylene Tetrafluoroethylene
FAA Federal Aviation Administration
FAR Federal Aviation Regulations
FOD
Foreign object damage
FL Flight Level
Fuse box
Power conditioning and distribution for the Engine Management
System
hr. hours
HIC A Harness Interface Connector A
HIC B Harness Interface Connector B
IAT Indicated Air Temperature
ICA Instructions for Continued Airworthiness
IFR Instrument Flight Rules
IFSD In-flight-shutdown
INJ 1–8 Injector 1–8
Effectivity: 916 i A / C24
Edition 0/Rev. 1
00–00–00
Page 7
December 01 2023
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