Page 12 2
nd
Edition – Rev 0
03-00
AIRPLANE GENERAL DESCRIPTION
Fuel System
The fuel system consists of with two aluminum fuel tanks integrated within each wing leading
edge.
In normal conditions, the engine-driven gear pump sucks fuel from the selected tank. Fuel
valve is located on cabin central tunnel: it allows to switch LH and RH tank. An electric fuel
pump supplies the engine in case of engine-driven pump failure.
On instrument panel there are other instruments: The fuel pressure indicator and fuel quantity
indicators.
FUEL TANK
ENGINE COMPARTEMENT
FUEL SELECTOR
ELECTRICAL PUMP
GEAR PUMP
ELECRIC FUEL PRESSURE SENDER
Figure 12: Fuel system layout
To Next Page
Loading...
