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

 

Engine	912 UL	912 ULS	912 iS
Power [hp]	80	100	100
Cruising speed [km/h] **	184	194	194
Max. speed [km/h] **	200	208	208
Stall speed [km/h] **	71	71	71
Rate of climb [m/s] **	4	5	5
Wing span [m]	8,71	8,71	8,71
Length [m]	6,38	6,38	6,38
Height [m]	2,20	2,20	2,20
Wing area [m²]	11,9	11,9	11,9
Empty weight * [kg]	281	285	294
Max. takeoff weight [kg]	560	560	560
Payload max. * [kg]	279	275	266
Fuel tank volume [l]	65	65	65
Take off distance [m]	120 – 140	100 – 120	100 – 120
Glide ratio	11	11	11
Data state 04.2019, technical changes reserved.
* Depends on interior
** Depends on interior and propeller.