l I.C.P. Sri l
Savannah
FLIGHT MANUAL l Pag.
10
l
1.8
ELECTRICAL SYSTEM
With reference
to
fig.2 on page
12,
the airplane's electrical system ineludes a 12V battery, a
generator, wiring and switches
to
supply and connect the engirre starter, an auxiliary fuel pump,
anti-collision and navigation lights, and the avionics. A voltmeter
is
provided
as
a standard
equipment.
The key-operatedmaster switch connects the electrical system
to
the 12V battery. The whole
electrical system
is
protected by thermal type re-settable breakers.
With the master switch OFF any electrical instrument and all other electrical devices,
electric
engirre starter included, won't be operating.
With reference
to
fig.
2:
A.
starter relais
B.
regulator
C.
electric fuel pump
D.
master switch
E.
power supply
F. elevator trim motor
G.
battery
4.
revolution counter supply
5.
hourmeter
6.
voltmeter
7.
left head temperature
8.
right head temperature
9.
o il temperature
l
O.
oil pressure
15.
low voltage waming lamp
18.
elevator trim switch
21-25 switches
26-27 breakers
1.9 CABIN
Two large lateral doors allow an easy indipendent access
to
the cabin. They are hinged by means
of
two hinges on the upper edge o f the doors , and may b e closed by a key handle located in the lo w er
edge and a latch in the front edge. The doors may be removed unscrewing the hinges bolt
as
required for flying in hot regions or
to
take pictures. Those windows MUST NOT be opened in
flight.
W ARNING: close latch in the front edge before flight.
Issue l/Revision 3
July'03
ICP
Sri-
Via Torino 12, 14020 PlOV
A'
MASSAIA
(AT)-
Italy
Phone +39-0141-996503
• Fax +39-0141-996506
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