There is an integral fuel tank in each wing (optionally 50 or 75
litres) positioned between the main and rear spar. Fuel gauges,
fuel lines (feed and return line) are installed in the structure. Drain
valves are positioned on the lowest point. Fuel tank ventilation
lines are integrated in the most outbound flap hinges.
The wing is optionally equipped by integral position lights at the
leading edge of wing tips. The wings can be dismounted for
transport or storage by removing two main pins and one rear wing
pin, dismounting flaps drive, ailerons control, fuel hoses and
electrical connectors.
Ailerons
The 40% differential ailerons with carbon monocoque structure are
hinged on three carbon hinges attached to the top wing shell. A
push-pull tubes and bellcrank are used for control.
Aerodynamic forces are relieved by automatic trim tabs.
Flaps
Fowler flaps with monocoque sandwich design are hinged on three
lever-hinges and driven by root-rib lever. The flap system is driven
by an electric motor and 4 positions are pre-programmed:
• FLAPS 0 0° flaps up
• FLAPS I 20° take-off
• FLAPS II 30° short take off/ landing
• FLAPS III 38° landing
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