l I.C.P. Sri j
Savannah
FLIGHT
MANUAL
Pag.
91
The master switch key is located near
to
the pilot's throttle. All the switches and the engine
controls commute to ON
if
moved UPWARD or FOREWARD. The mixture control only, is
activated pulling it BACKWARD.
1.6
PROPELLER
The aircraft features the foliowing propeller:
"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.
1.7
FUEL SYSTEM
With reference
to
fig. l on page
11,
the fuel system is equipped with two tanks (1, 2). They
are
instalied into the wings and have a
72
lt.
capacity. The filler caps inelude a vent hole. The
reservoirs features an overcapacity fuel pipe ending below the wing. The left fuel tank is with a
visual fuel level indicator located on left wing first rib. The drain valve (5.) is located in the fuel
bowl (3.) instalied in the fuselage, o n the right side; a fuel reserve warning is instalied o n the bowl
to indicate low remaining fuel. A fuel valve is fitted (7.): this fuel valve is held in the OPEN
position by a safety wire. That safety wire can be broken in an emergency. This safety wire must be
used to prevent an accidental in-flight fuel valve elosure leading to an engine shut-down or, even
worse,
to
a elosed fuel valve take-off. The fuel pump (8.) is mechanically cams operated. A fuel
pressure gauge is installed.
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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