d
065
15.
fm
SI-PAC-001
SERVICE INSTRUCTION -
PAC
08 February 2019
24-30-00
Initial Issue
Page 7 of 21
Copyright - BRP-Rotax GmbH & CO KG. All rights reserved.
Wiring dia-
gram
Fig. 3. External alternator
.
Fuse Box
Regulator board A
Regulator board B
ECU
1
2
3
Battery
Master
switch
Circuit breaker
(30
A)
AWG
12
AWG
12
Backup battery switch
(guarded switch)
24
3
1
Start power switch
(momentary)
1
2
3
4
AWG
12
AWG
12
AWG
12
A
AWG
04
AWG
12
X3
M
Start Relais
E-Starter
AWG
12
AWG
12
V
912
iS wiring harness
Airframe Ground
EMS ground
AWG 04 (21,1 mm²)
AWG 12 (3,3 mm²)
AWG 16 (1,50 mm²)
AWG 18 (1,00 mm²)
AWG 20 (0,75 mm²)
Optional
(not required
)
Circuit breaker
(30
A
)
AWG
06
AWG
08
AWG
08
AWG
12
B
G
L
External
alternator
Circuit breaker
has to
be provided by the
aircraft manufacturer
AWG
12
Indicator
lamp
Circuit
breaker
(5
A)
Circuit breaker
(Max.
850
W when using an
external alternato
r)
Circuit breaker
(50
A)
!
lternator
FIELD
switch
08255
Bus bar (Airframe)
08255
