2-person ULM aircraft C42 C

4-stroke enginetouristsingle-engine

The IKARUS C42C is an innovative development based on the proven IKARUS C42 series – high-performance EH airfoil with GRP sandwich-reinforced leading edge – standard wind tunnel and CFD flow simulation optimized winglets – better control comfort with Spades and Flettner rudder – better engine cooling due to lightweight tubular frame engine support made of high-strength performance steel – improved cockpit seals through redesign of the windscreens and door integration – aerodynamic optimisation of the fuselage – landing flap transition through gap claddings Areas of application Used for flight schools, as a touring aircraft, as a tow plane. Can be equipped with a Rotax 912iS engine and a Rotax 914 Turbo. Optional with floats or skis. Standard equipment for C42 C 80 HP Rotax engine | rescue system | stainless steel exhaust system | hydraulic disc brakes with parking brake | comfortable and effective cabin heating | carburettor preheating | airbox with Naca inlet | covering with extra protective film against UV rays | inspection-friendly wing and cowling locks | large luggage compartment opening | cabin locks with new high-security designer door handles | adjustable air inlets in both doors | incl. basic flight instruments, engine instruments, decorative strips | digital, precisely readable tachometer with engine time recording | can also be equipped with the special version for pilots in a wheelchair plus – Tubular engine mount – Spades – Flettner-rudder – Gap cladding between landing flaps and fuselage for reduction of turbulences – Light winglets made of honeycomb sandwich – Electric elevator trim with stick actuation – Strut connection cladding