7. TECHNICAL DESCRIPTION OF THE
AIRPLANE
SHARK is a composite high-performance low-wing airplane with tandem
seats and retractable tricycle type undercarriage, designed according to
European UL and US Light Sport Airplane criteria.
Airplane is powered by 100HP Rotax 912ULS with variable-pitch
composite propeller and 100/150 litres integral fuel tanks in the wings.
EQUIPMENT: Shark is equipped by upholstered two-seat tandem cockpit
with adjustable seats, full dual control (with sidesticks on the right) and
throttle levers on the left panels.
Elevator trim tab, radio and autopilot OFF button are placed on sidesticks.
Instrument panel: equipped by standard EFIS/EMS displays for both
pilots has control panel for landing gears, flaps, propeller, transceiver,
transponder and optionally GPS, ELT and backup flight indicators.
The single-piece cockpit canopy: supported by gas struts, opens to
starboard.
Baggage compartment: is located behind the rear seat, accessible from
the rear pilot seat or through lockable baggage door on the left side of the
plane.
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