Rotax 24-30-00, Service Instruction

Page: 17 / 21

d
065
15.
fm
SI-PAC-001
SERVICE INSTRUCTION -
PAC
08 February 2019 24-30-00
Initial Issue Page 17 of 21
Copyright - BRP-Rotax GmbH & CO KG. All rights reserved.
3.5) Connecting the external alternator into the electric circuit
There are two options for connection of the external alternator:
OPTION A : Connection to main switch at battery. See Fig. 18 .
Fig. 18
Step OPTION A - Procedure
1 Connect alternator terminal “B” to the main switch at the battery with a flexible multi-
strand wire with proper cross-section according to the requirements in the relevant
aircraft installation and a 50 A fuse.
2 Connect terminals “IG” and “L” into the circuit in accordance with the wiring diagram
(
Fig. 3 ) using connectors and housing provided.
L
B
IG
L = Terminal “L”
IG = Terminal “IG”
B = Terminal “B”
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