ICP Savannah VG User Manual

I.C.P. Srl Savannah™VG FLIGHT MANUAL
Pag. 10
Issue 1/Revision 03
ICP Srl – S.P.16 km 15,150 14022 Castelnuovo Don Bosco (AT)
Jan.2012 Tel. 011.9927503 Fax 011.9927266
1.6 PROPELLER
One of the following propellers may be installed on this airplane:
- “DUC Helice”, 3 blades in carbon fiber (Rotax 912 ULS), adjustable on ground.
- “DUC Helice”, 2 blades in carbon fiber (Rotax 912 UL), adjustable on ground.
- 2 BLADES IN CARBON FIBER (Jabiru2200)
1.7 FUEL SYSTEM
With reference to fig. 1 on page 11, the fuel system is equipped with two tanks (1, 2). They
are installed in the wings and have a 72 lt (19 gal) capacity. The filler caps have a vent hole. The
reservoirs have an overcapacity fuel pipe ending below the wings. The left fuel tank has a visual fuel
level indicator located on left wing first rib. The drain valve (5) is located in the fuel tank behind the
right seat (3). A fuel reserve warning light is installed to indicate low remaining fuel in the collector
tank behind the seat. The installed fuel valve (7) is held in the OPEN position by a safety wire. That
safety wire can be broken in an emergency. This safety wire is used to prevent an accidental in-flight
fuel valve closure leading to an engine shut-down or, even worse, to a closed fuel valve take-off. The
fuel pump (8) is mechanically operated by the engine, a fuel pressure gauge is installed to check the
system operation.
1.8 ELECTRICAL SYSTEM
With reference to fig.2 on page 12, the airplane’s electrical system includes a 12V battery, a
generator, wiring and switches to supply and connect the engine starter, an auxiliary fuel pump, anti-
collision, navigation lights and the avionics. A voltmeter is provided as a standard equipment.
The key-operated master 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
engine starter included, will not operate.
With reference to fig. 2:
A. starter relay
B. voltage regulator
C. electric fuel pump
D. master switch
E. power supply (aux)
F. elevator trim motor
G. battery
4. RPM gauge
5. hourmeter
6. voltmeter
7. left head temperature
8. right head temperature
9. oil temperature
10. oil pressure
15. low voltage warning lamp
18. elevator trim switch
21-25 switches

ICP Savannah VG Specifications

General

Brand	ICP
Model	Savannah VG
Category	Aircrafts
Language	English