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OPERATING AND MAINTENANCE MANUAL FOR ULTRALIGHT AEROPLANE
2.3.7. Power plant control
The engine power is controlled by a throttle lever located on the instrument panel, in the
panel center line. There are the two bowden cables led from the throttle lever to the
carburetors.
To start could engine the carburetors are equipped with a chords controlled by a lever
located below the instrument panel. The ignition switches are located on the instrument
panel. Switch on the ignition and the turn key in the in the switch box to start the engine.
2.3.8. Fuel system
The airplane is equipped with two 50 liters ( each ) fuel tanks in both wings.
The fuel tank filler neck is placed on the wing upper surface and equipped with a cap sealed
by a packing "O" ring. A fuel tank bleeding hole is located on the wing tip. A fuel tank
draining valve is located under the wing in the lowest part of the fuel tank. Use the valve to
empty the fuel tank, also.
Fuel is pulled in the fuel tank through the fuel tank outlet coarse screen. Then through the
fuel valve and fine screen to the fuel pump and on he carburetors. Fuel quantity is indicated
by an automotive fuel gauge located on the instrument panel. There is installed a float in
the fuel tank to scan a fuel quantity. The fuel gauge displays the relative quantity of fuel
inside the fuel tank, corresponding fuel quantity liters is shown on the placard "WEIGHT"
in the cockpit.
Document No:
Date of issue: 30.01.2008
UFM-13 Lambada
2-9
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