TOMARK Viper SD-4 RTC - Flight Controls; Control Surface Deflections

TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 27 Flight Controls
Page 98 Issue: 11.AUG 2016
27 Flight Controls
The airplane is equipped with a complete dual control system for
elevator, aileron and rudder. Standard control elements - control stick
and rudder pedals - are used for aerodynamic control.
The control sticks control the ailerons and the elevator. The foot
control pedals control the rudder and the front landing gear wheel.
The wing flaps are actuated electrically by a lever-type controller.
Control Surface Deflections
Aileron deflection angle
up +27° ± 1°
down -16° ± 1°
Elevator deflection angle
up +25° ± 1°
down -20° ± 1°
Flap deflection angle
0° ± 2°
15° ± 2°
30° ± 2°
[40°
1
± 2°]
Rudder deflection angle
left +30° ± 1°
right -30° ± 1°
Elevator’s trim tab
deflection angle
up +21° ± 2°
down -33° ± 2°
Aileron´s trim tab
deflection angle
up +28° ± 2°
down -28° ± 2°
Table 2 Control surface deflections
1
Not used for normal operation