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nd
Edition – Rev 0
27-10
FLIGHT CONTROLOS - GENERAL
27- 10 FLIGHT CONTROLS – GENERAL
DESCRIPTION AND OPERATION
The aircraft is controlled in flight by the use of the three standards primary control surfaces:
stabilator, rudder and ailerons.
Control devices are of conventional type; a double system of control axis and pedal is
provided
The wing flaps are electrically operated and can be positioned in any locations up to 40°.
Figure 1. - Flight controls
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