C42 B

The allrounder

MTOW: 540 kg

Approval as: LTF-UL 2019 / BCAR S / ASTM LSA

Features of the C42 B

 

The C42B is equipped with significant product enhancements, detail optimizations and material improvements. The C42B is used in most flight schools as a training aircraft and with its good-natured flight characteristics it is also suitable for beginners. As a tow plane the C42B is equipped with a larger counter flow heat exchanger which provides optimal cooling conditions.

Areas of application

 

Used for flight schools, as a touring aircraft, as a tow plane and as a crop-spraying plane. Can be equipped with a 912iS engine as well as a 914Turbo. Optional with floats, skis or with a wing folding device.

Standard equipment for C42B

 

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.

C42 B Technical data

 

Engine 912 UL 912 ULS
Power [hp] 80 100
Cruising speed [km/h] ** 168 178
Max. speed [km/h] ** 183 191
Stall speed [km/h] ** 69 69
Rate of climb [m/s] ** 4 5
Wing span [m] 9,45 9,45
Length [m] 6,38 6,38
Height [m] 2,20 2,20
Wing area [m²] 12,5 12,5
Empty weight * [kg] 276 280
Max. takeoff weight [kg] 540 540
Payload max. * [kg] 264 260
Fuel tank volume [l] 65 65
Take off distance (grass) [m] 120
– 140		 100
– 120
Gleitzahl Glide ratio 11 11
Data state 04.2019, technical changes reserved.
* Depends on interior
** Depends on interior and propeller.