Garmin G950 IFDS - Supplement
Page S7 - 42
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
4
th
Edition, Rev. 0
The following loads are connected to the battery bus:
In addition, directly on the battery, the following devices are connected:
• Emergency back-up attitude indicator (RH attitude indicator – usually supplied
from RH generator bus), when installed;
•
Emergency Light
•
Chronometer
The first two devices are controlled by the pertinent switches located on the LH
breakers rack.
Battery Bus
GMA 1347 Audio Panel
GIA #1
GDU PFD
Cooling Fan
Converter 1
Standby attitude indicator
LH and RH Fuel electrical pump
LH and RH Fuel pressure
LH and RH Fuel quantity
LH and RH Oil pressure
LH and RH Oil temperature
LH and RH CHT
LH and RH RPM indicator
Cabin lights
Cockpit lights
Switches built-in lights
Avionics lights
Strobe lights
Flaps
Doors pressure switches
Engine hour meter (2 units)
Turn coordinator (A/P slaved)
LG hydraulic pump
LG indicating & control system
LH and RH Fire detector
Chronometer
12V cabin electrical power sockets (2
units)
Summary of Contents for P2006T
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