SECTION 7
DESCRIPTION OF
AIRPLANE AND SYSTEMS
PS-POH-1-1-01
Date of issue: 10/03/31
Revision: -
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.
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 bulkhead, on the gascollator.
Fuel selector valve is on the central console in the cockpit.
The electric fuel pump is located on bulkhead 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).
Left green mark Right green mark
NOTE
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.
CAUTION
Do not overfill the tanks to avoid fuel overflow through venting tubes.
Summary of Contents for Piper Sport
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