The fastest in the IKARUS series
MTOW: 472.5 kg (constructive design for 560 kg)
Approval as: LTF-UL
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
– Engine frame carrier
– 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
Data status: April 2018 – subject to change.
Technical data are partly approximate values.