C42 CS
The fastest in the IKARUS series
MTOW: 560 kg
Approval as: LTF-UL 2019
Features of the C42 CS
The IKARUS C42CS is an innovative further development based on the proven IKARUS C42C.
The well-known innovations and technical developments already implemented in our successful C42C are rounded off by the composite single-swing landing gear and is the logical further development to the standard sports aircraft.
The aerodynamically high-quality landing gear offers a significantly higher cruising speed. Thus, sporty and pleasant traveling complement each other to a perfect flying experience.
Areas of application
Wird eingesetzt für Flugschulen, als Reiseflugzeug, als Schleppflugzeug.
Kann mit einem Rotax IS Motor ausgestattet werden.
Standard equipment for the C42 CS
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 | cover 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 taxiing stall
plus
– Engine frame carrier
– Spades
– Flettner-rudder
– Gap fairing between flaps and fuselage
– Electric elevator trim with stick actuation
– Strut connection cladding
– Aerodynamic single swing composite landing gear
– High quality Beringer brake including parking brake
C42 CS Technical specifications
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Injection |
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Power |
80 PS |
100 PS |
100 PS |
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Cruising speed 75% |
184 km/h |
194 km/h |
194 km/h |
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Maximum speed Vmax |
200 km/h |
208 km/h |
208 km/h |
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Stall speed VS0 |
71 km/h |
71 km/h |
71 km/h |
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Rate of climb |
4 m/s |
5 m/s |
5 m/s |
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Wing span |
8,71 m |
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Lenght |
6,38 m |
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Height |
2,20 m |
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Wing area |
11,9 m² |
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Max. take-off weight / MTOW |
560 kg |
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Empty weight incl. rescue system BRS |
281,5 kg |
285,5 kg |
293,8 kg |
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Load capacity |
278,5 kg |
274,5 kg |
266,2 kg |
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Tank capacity |
65 Liter |
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Consumption liters/hour |
11 - 14 |
12 - 15 |
11 - 14 |
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Range with 65 liter tank |
approx. 780 km |
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Take-off roll distance (grass) |
120-140m |
100-120m |
100-120m |
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Glide ratio |
11 |
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