Rotax 915 i A SERIES Maintenance Manual page 17

DC
DOA
DOT
EASA
IM
ECU
EGT
INTRO
EMS
EN
ETFE
FAA
FAR
hr.
HIC A
HIC B
IFR
INJ 1–8
IPC
ips
iRMT
ISA
kg
KNOCK
MAPS 1+2
MATS 1+2
MON
MAG
N
n.a.
NDT
Nm
Effectivity: 915 i A Series
Edition 0/Rev. 0
BRP-Rotax
MAINTENANCE MANUAL
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
Instrument Flight Rules
Injector 1–8
Illustrated Parts Catalog
inch per second
independent ROTAX Maintenance Training
International Standard Atmosphere
Kilograms
Knock sensor
Manifold Air Pressure Sensor 1+2
Manifold Air Temperature Sensor 1+2
Motor Octane Number
Magneto Side
Newton
not available
Non Destructive Testing
Newtonmeter
00–00–00
Page 5
December 01 2017