An exemplary high-lift system for an aircraft includes a wing, a high-lift flap coupled to the wing, a kinematic element which is driven by a drive device, and a flap lever structured and arranged to rotate via an actuating drive between a retracted position in which the high-lift flap complements a wing profile and a plurality of extended positions in which a slot of a given width is formed between the wing and the high-lift flap. A first end of the flap lever is coupled to the high-lift flap. A second end of the flap lever is coupled to the kinematic element and is capable of rotating relative thereto via a first rotation point. The kinematic element is structured and arranged to rotate relative to a second rotation point that is fixed in position relative to the wing. The first rotation point is separated by a predetermined distance from the second rotation point.
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