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TOMARK Viper SD-4 RTC - Flap System Operation

TOMARK Viper SD-4 RTC
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TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 27 Flight Controls
Page 110 Issue: 11.AUG 2016
27-50 Flap System
The electric actuator located under the pilot’s seat drives a common
torque tube extending/retracting left and right side symmetrically.
Flaps can be operated into 4 positions (refer to Table 2).
Figure 14 Flap system
Item
Description
Item
Description
1
Flap
3
Bell crank
2
Electric actuator
4
Torque tube
The flaps are controlled by a guarded lever-type electric controller,
located on the central panel between the pilot seats. By pushing the
lever to the right and moving it for or aft, the desired flap position
can be achieved.

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