Abbrevia-
tions
Description
CSA Constant Speed Actuator
CTS Cooling Temperature Sensor
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 in-
tended to be disconnected 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
Page 1-4
December 01 2023
BRP-Rotax Effectivity: 916 i A / C24
Edition 0 / Rev. 1