Rotax 912 i Series Maintenance Manual page 18

DCDI
DC
DOA
DOT
EASA
IM
ECU
EGT
INTRO
EMS
EMC
EN
ETFE
FAA
FAR
FOD
hr.
HIC A
HIC B
IAT
ICA
IFR
IFSD
INJ 1–8
IPC
ips
iRMT
ISA
kg
KNOCK
LOPC
MAPS 1 & 2
00–00–00
Page 6
September 01/2018
BRP-Rotax
MAINTENANCE MANUAL LINE
Dual Capacitor Discharge Ignition
direct current
Design Organisation Approval
Department of Transport
European Aviation Safety Agency
Installation Manual
Engine Control Unit
Exhaust Gas Temperature
Introduction
Engine Management System
Electromagnetic compatibility
European Norm
Ethylene Tetrafluoroethylene
Federal Aviation Administration
Federal Aviation Regulations
Foreign object damage
hours
Harness Interface Connector A
Harness Interface Connector B
Inorganic Additive Technology
Instructions for Continued Airworthiness
Instrument Flight Rules
In-flight-shutdown
Injector 1–8
Illustrated Parts Catalog
inch per second
independent ROTAX Maintenance Training
International Standard Atmosphere
Kilograms
Knock sensor
Loss of power control
Manifold Air Pressure Sensor 1 & 2
Effectivity: 912 i Series
Edition 2/Rev. 0