Horizontal stabilizer
The stabilizer has carbon monocoque sandwich design with
continual rear spar and auxiliary front spar. Hinges for the elevator
are attached on the top shell. The stabilizer is attached to fuselage
by two hinges on the rear fin frame and by one on the rear
fuselage bracket.
Elevator
The split monocoque elevator is attached to the stabilizer by 3
hinges. The left part is equipped with an electric trim-tab
controlled by a three position centrally-sprung switch on the side-
stick.
Rudder
The carbon monocoque rudder is hinged by two hinges and
controlled through steel wires by a lever placed below the root rib.
Airplane exterior surface painting;
White two-component acrylic polyurethane topcoat is used.
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