FIELD: transport.
SUBSTANCE: invention relates to the field of aviation, more specifically to a method for balancing fuel reserve in aircraft wing tanks during ground operation. The method consists in the following: balancing is executed via fuel pumping from the wing tank which contains more fuel to the central tank of an aircraft. In this process, to compensate a difference in fuel reserve between wing tanks the aircraft pump for fuel supply from left wing tank is switched on, centralised dump valve and central tank filling valve is opened, and fuel is fed under pressure to the central tank through central tank filling valve. Minor fuel part is returned from the central tank to the left wing tank by fuel jet pump.
EFFECT: prevention of transverse imbalance between left and right wing tanks.
4 cl, 1 dwg
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