Tecnam P2006T, Aircraft Flight Manual

Page: 237 / 508

Garmin G950 IFDS - Supplement
Page S7 - 43
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
4
th
Edition, Rev. 0
The other loads are so divided among following busses:
LH GEN Bus LH Avionic Bus RH GEN Bus RH Avionic Bus
Pitot heat DME NAV lights ADF
Landing light Transponder Rudder trim COM 2
Taxi light Encoder altimeter Stall warning NAV 2
RH attitude indicator A/P (*)
A/P Pitch Trim (*)
(*) if installed
On the central pedestal (see Figure below) there are seven switches disposed on
two rows: on the first row there is the MASTER SWITCH which allows for con-
necting, through the battery relay, the battery to the battery bus.
LH and RH FIELD switches control the pertinent generator: setting the switch to
OFF puts the pertinent generator off-line.
In correspondence of the second row there are 4 switches LH/RH AVIONIC and
LH/ RH CROSS BUS.
Central pedestal switches console
The first two allow, through a relay, for cutting off the power supply to the perti-
nent avionic bus.
The second ones allow, through a relay, for realizing the parallel connection be-
tween the pertinent generator bus and the battery bus. Setting these ones to OFF,