The article describes specific features of the aircraft aerodynamic configuration aimed at the excellent wing lifting capacities and favourable stall characteristics. Some details concerning the automated primary flight control system operating algorithms to provide the required handling characteristics and the aircraft pro-tection against stall development are presented. It is shown that the aircraft attains the designed maximum lift coefficient, displays the favourable stall performance and the desired anti-stall protection.

The World Congress "Aviation in the X X I-st Century", 14-16 september [Текст] = Матеріали Всесвітнього конгресу "Авіація ХХІ століття" 14-16 вересня 2003 року / International Civil Aviation Organization; Ministry of Education and Science of Ukraine; National Academy of Sciences of Ukraine; National Aviation University. — Kyiv : NAU, 2003. — 438 p. : il.