Pipistrel VIRUS SW 600 D, Pilot Operating Handbook

Page: 92 / 98

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PAGE
Virus SW 600 D
iS engine
POH Supplement
SPOH-127-00-41-001
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SECTION 7
AIRPLANE DESCRIPTION
Electrical supply from generators and battery is distributed to the following:
Equipment (example)
Electrical Consumption
[A] @ 14 V
Typical configuration: Dynon Skyview avionics
system which includes display HDX1100 (PFD), 1x
SV-BATT320 backup battery, Dynon EMS (EIS), 1x
Dynon ADAHRS, sensors.
~3.7 A total (See OEM
of each device for
individual electrical
consuption data)
COM and transponder (Funke/Air Avionics)
See OEM of each
device for individual
electrical consuption
data
Landing light 5 A
Nav lights 0.27 A
Strobe lights 0.44 A
Electrical trim 0.3 A
NOTE: See OEM of each device for individual electrical consuption data.
7.8.4 SWITCHES
Master Switch
The MASTER toggle switch is installed on the switch panel and activates the
relay to connect the battery with main bus. Main bus supplies the avionics
relay which delivers the power to the switch panel and circuit breakers. To
check or use avionics equipment or radios while on the ground, the AVION-
ICS power switch must also be turned on. The 12V socket is connected via
switch/fuse directly to the main battery.
Avionics Power Switch
A toggle switch, labeled AVIONICS, controls electrical power from the main
bus to the Avionics Bus. The switch is located next to the MASTER switch.
Typically, the switch is used to energize or de-energize all avionics on the
Avionics Bus simultaneously. With the switch in the OFF position, no elec-