d05395.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 1
74-00-00
Page 1
July 01/2012
Chapter: 74-00-00
IGNITION SYSTEM
Introduction The ignition system is powered by the ECU and has fully mapped varia-
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: All components are installed on the aircraft engine as stan-
dard.
Table of contents This section of the Installation Manual contains information on the aircraft
engine ignition system.
Subject Page
Connection to rectifier regulator Page 3
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