C 42 Portrait
C42 Series - the bestseller, meanwhile more than 1200 units delivered worldwide -the bestselling ultralight aircraft in Germany
Maximum fun of flying at a reasonable ratio between price and performance.
An innovative, modern two-seater micro-light aircraft sets the standards. The classic advantages of the ultralight and the standard aircraft categories are combined to produce a fascinating, technically matured machine.
The IKARUS C42 Series is very popular due to its excellent flight characteristics.
- The aluminium tube construction combined with carbon fibre, Aramid and glass fibre enables light weights at high solidity
- This way of construction is also very maintenance-friendly
- Optimised engine performance and low fuel consumption by the use of separate supplies for fresh air with the aid of NACA-intake with charge effect
- The oil cooler integrated into the cooling water circuit guarantees ideal set-up between oil-, water- resp. cylinder head temperature
- Additional preheating prevents carburettor icing
- A climate of wellness due to cabin heating and air vent
- Standard electric trim and landing flap adjustment
- Optional aerodynamic main gear fairing
- The standardl Carbon fibre winglets cause an elegant visual effect and even better flight characteristics at low speed flight as well as at banner- and aero-tow
- Aerodynamic design of the engine-cowling and front-screen-tilting has been optimised in the wind tunnel
- The high opening folding doors reach all down to the cabin floor. They allow the most comfortable entrance into the 1,2 m wide, spaciously glassed cabin.
- Over-average high payload
- Affordable Aero-tow up to 650 kg towing capacity
Technical data C42E 100HP
Cruising speed (IAS) | 175 km/h | Wing area | 12,5 m² |
Max. airspeed Vmax (IAS) | 190 km/h | MTOW* | 540,0 kg |
Stallspeed | 65 km/h | Fuel tank volume | 65 Liter |
Rate of clim (472,5 kg) | 5,0 m/s | Average consumptionof fuel L/hr | 12-17 |
Wing span | 9,45 m | Range 65 Liters tank | ca. 700 km |
Length | 6,38 m | Length of takeoff run (Gras) | 90-100m |
Height | 2,20 m | Glide ratio | 11 |
* MTOW and payload may be different according to national law"