FIELD: aircrafts. SUBSTANCE: aileron control system is provided by the additional rigid kinematic link 8, preventing spontaneous deflection of ailerons 1 and the balance tabs in dependance upon an attack angle at fixed position of the control lever 2. EFFECT: lowered moment of hinge-joint rotation of ailerons due to increased efficiency of balance tabs at large attack angles. 1 cl, 1 dwg
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