SC-POH-1-1-17
SECTION 7
DESCRIPTION OF
AIRPLANE AND SYSTEMS
Revision: -
Date of issue: 2011-09-01
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7-6
7.10 Canopy
Access to the cabin is from both sides. Make sure that the canopy is latched
and mechanism is securely locked into position on both sides before operating
the aircraft and manually check the canopy is locked by pushing the canopy
upward. The canopy unlocked indicates
CABIN OPENED
red LED flashing
placed on upper left part of instrument panel.
7.11 Fuel system
Each tank is equipped with a vent outlet, finger screen filter and float sensor.
Drain valve located in the lowest point of the each tank and on the bottom
edge of the firewall, on the gascolator. Fuel selector valve is on the central
console in the cockpit. The electric fuel pump is located on firewall and it is
used for fuel line filling before engine starting. Fuel return hose goes from the
fuel pump into the left tank.
CAUTION
During operation, fuel valve shall be in
LEFT
or
RIGHT
tank position
(position on green mark).
NOTE
Fuel is not closed when the fuel valve is in upper half between
LEFT
and
RIGHT
tank
positions.
If left tank is full, start engine with the fuel selector set to
LEFT
. If you would start the
engine with the fuel selector set to
RIGHT
and the left tank is full, than fuel bleed
from the left tank vent may occur because a fuel return hose is led only into the left
tank and returning fuel will overfill the left tank.
