Rotax 915 i A series Maintenance Manual page 359

INSTALLATION
Preparation
ATTENTION
The wire connectors of the ECU must not be
opened and closed more than 20 times! This
must be shown on the device by a clearly visi-
ble label with a printed numerical sequence (1-
20) and by documentation conforming to self-
monitoring guidelines.
NOTE
The ECU can only be replaced as a complete
spare part.
ECU - INSTALLATION
ATTENTION
Installation must be carried out according to
the aircraft manufacturer's and to the specifi-
cations of the Installation Manual.
Step Procedure
1 Install the control unit according to the air-
craft manufacturer's instructions.
2 Plug the wiring harness (main strand) into
the ECU and turn lever.
• Plug in connector LANE A1
• Plug in connector LANE A2
• Plug in connector LANE B
NOTE
Ensure that the correct connection is made to
the corresponding LANE by using the white line
marking.
Step Procedure
3 Install the battery grounding cable ac-
cording to the aircraft manufacturer's
instructions.
Effectivity: 915 i A Series
Edition 0/Rev. 0
BRP-Rotax
MAINTENANCE MANUAL HEAVY
Figure 15.7
Connector (LANE A1)
1
Connector (LANE B)
3
NOTE
Put the lever completely horizontal, place on the
connector, then close the lever 90°. The lock
must latch.
Figure 15.8
1 Lock 2 Lever
Connector (LANE A2)
2
76–10–00
Page 9
August 01 2018