BRP Rotax 915 i A Series Maintenance Manual page 18

DCDI
DC
DOA
DOT
EASA
IM
ECU
EGT
INTRO
EMS
EMS GND
EMC
EN
ETFE
FAA
FAR
FOD
Fuse box
hr.
HIC A
HIC B
IAT
ICA
IFR
IFSD
INJ 1–8
IPC
ips
iRMT
ISA
00–00–00
Page 4
June 01 2019
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
Engine system internal ground reference which is intended to be dis-
connected from aircraft common ground during flight
Electromagnetic compatibility
European Standard
Ethylene Tetrafluoroethylene
Federal Aviation Administration
Federal Aviation Regulations
Foreign object damage
Power conditioning and distribution for the Engine Management
System
hours
Harness Interface Connector A
Harness Interface Connector B
Indicated Air Temperature
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
Effectivity: 915 i A Series
Rev. 1