Tecnam P2006T - Page 223

Page 7 - 41
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
4
th
Edition, Rev 0
The following loads are connected to the battery bus:
Battery Bus
Audio Panel
VHF COMM 1
NAV 1
GPS
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
LH Attitude indicator
Cabin lights
Cockpit lights
Switches built-in lights
Avionics lights
Annunciator Panel
Strobe lights
Flaps
Doors pressure switches
Engine hour meter (2 units)
OAT
Turn coordinator
LG hydraulic pump
LG indicating & control system
LH and RH Fire detector
12V cabin electrical power sockets (2
units)
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.