d
065
15.
fm
SI-PAC-001
SERVICE INSTRUCTION -
PAC
08 February 2019
24-30-00
Initial Issue
Page 5 of 21
Copyright - BRP-Rotax GmbH & CO KG. All rights reserved.
3.1) Installation - related information
Optional
extras
-
External alternator (as option if the output of the integrated generator is inadequate).
3.1.1) Technical data
General note
NOTE:
The voltage regulator is integrated in the alternator.
Output
Max. 550 W/DC at 6000 r.p.m. (complies ~ 4800 r.p.m. crankshaft speed).
Output voltage
14.2 V - 14.8 V.
Ambient temp.
Ambient temperature range
:
Weight
Weight: 3.0 kg (6.61 lbs).
3.1.2) Connections
Power supply
wires
Power supply wires to external alternator (1) have to be installed depending on the mounting posi-
tion and according to the regulations of the aircraft manufacturer.
Positive termi-
nal
Positive terminal (2):
M6 screw connection suitable for cable terminal according to DIN 46225 (tightening torque 4 Nm
(35 in. lb)).
Ground
Via engine block.
Control wiring
Control wiring (3): Via supplied standard plug (Sumitomo 6111-2568) and 6.3x0.8 Faston connec-
tors (female).
Fig. 1.
Min.
Max.
-30 °C (-22 °F)
+90 °C (194 °F)
IG
L B
Cyl. 1
Cyl. 3
Cyl. 2
Cyl. 4
1 External alternator
2 Positive terminal
3 Control wiring
1
03199
