Rotax 915 i A series Maintenance Manual page 25

DCDI
DC
DOA
DOT
EASA
IM
ECU
EGT
INTRO
EMS
EN
ETFE
FAA
FAR
hr.
HIC A
HIC B
IAT
IFR
IFSD
INJ 1–8
IPC
ips
iRMT
ISA
kg
KNOCK
LOPC
MAPS 1 & 2
MATS 1 & 2
MON
MAG
Effectivity: 915 i A Series
Edition 0/Rev. 0
MAINTENANCE MANUAL HEAVY
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
European Norm
Ethylene Tetrafluoroethylene
Federal Aviation Administration
Federal Aviation Regulations
hours
Harness Interface Connector A
Harness Interface Connector B
Inorganic Additive Technology
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
Manifold Air Temperature Sensor 1 & 2
Motor Octane Number
Magneto Side
BRP-Rotax
00–00–00
Page 5
August 01 2018