Rotax 912 i Series Installation Manual page 113

The ignition system is powered by the ECU and has fully mapped varia-
Introduction
ble timing. It is completely doubled up. Either of the ECU's can operate
the double ignition coils. If a fault occurs with the ignition system the ECU
informs the pilot by warning lamps through the display in the instrument
panel.
NOTE:
This section of the Installation Manual contains information on the aircraft
Table of contents
engine ignition system.
Connection to rectifier regulator
Effectivity: 912 i Series
Edition 1/Rev. 1
BRP-Powertrain
INSTALLATION MANUAL
Chapter: 74-00-00
IGNITION SYSTEM
All components are installed on the aircraft engine as stan-
dard.
Subject Page
Page 3
74-00-00
July 01/2012
Page 1