FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to method of equalising fuel capacity in aircraft wing tanks. Proposed method consists in that equalising is performed by pumping fuel from aircraft central tank into wing tank with smaller fuel capacity. Note here that valves for feeding fuel to engines and cross valve stay in "shut-off" position to feed fuel from central tank via fuel transfer jet pump into wing tank sump compartment to feed therein an amount of fuel required for balancing fuel amount in both wing tanks.
EFFECT: ruling out unbalance between left and right wing fuel tanks.
2 cl, 1 dwg
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