Document: SLSA-MIP-5-4-0-US
Date of Issue: 05/2016
Revision: -
6-5
6.2.4
Elevator trim tab control
The elevator trim tab is controlled by the electrical actuator installed in elevator and
connected per threaded rod with trim tab. Control switches are integrated part of grip on the
left control stick (option on both control sticks). A LED position indicator is installed on the
instrument panel.
Fig. 6-4
Trim tab control
6.2.5
Wing flap control
Wing flaps are controlled by an electric flaps actuator connected with flaps per torque tube
with push rods on each end. The flaps actuator is located in center channel of fuselage
between the seats and is controlled by programmable control unit and three positions switch
located on instrument panel. A LCD indicator is installed in control unit for easier programing
of the positions. It is possible to set the wing flaps to 3 or 4 positions in range from 0
° to 30°.
Company setting is 0°, 10°, 20° and 30°.
Fig. 6-5
Wing flap control
Summary of Contents for S-LSA
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