Rotax 912 i Series Installation Manual page 95

The ignition system consists of an internal alternator, crankshaft position
Introduction
sensors (2 pcs.), dual ignition coil (4 pcs.), ignition cable assy., resis-
tance spark plug connector (8 pcs.) and the spark plugs (8 pcs.). The
energy required to generate the spark is supplied via the internal alterna-
tor - regulator - FUSE BOX. The correct ignition timing point is controlled
by the ECU with the help of the rev. counter.
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. 0
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
January 01/2012
Page 1