BRP-Rotax
MAINTENANCE MANUAL LINE
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
EMC
Electromagnetic compatibility
EN European Norm
ETFE
Ethylene Tetrafluoroethylene
FAA Federal Aviation Administration
FAR Federal Aviation Regulations
FOD
Foreign object damage
hr. hours
HIC A Harness Interface Connector A
HIC B Harness Interface Connector B
IAT Inorganic Additive Technology
ICA Instructions for Continued Airworthiness
IFR Instrument Flight Rules
IFSD In-flight-shutdown
INJ 1–8 Injector 1–8
IPC Illustrated Parts Catalog
ips inch per second
iRMT
independent ROTAX Maintenance Training
ISA International Standard Atmosphere
kg Kilograms
KNOCK
Knock sensor
LOPC Loss of power control
MAPS 1 & 2 Manifold Air Pressure Sensor 1 & 2
00–00–00
Page 6
September 01/2018
Effectivity: 912 i Series
Edition 2/Rev. 0
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