GET TO KNOW OUR AIRCRAFT
Ikarus C42
Model: C42B
Engine Options: Rotax 912 UL (80 hp) or Rotax 912 ULS (100 hp)
Cruising Speed: 168 km/h (80 hp) / 178 km/h (100 hp)
Maximum Speed: 183 km/h (80 hp) / 191 km/h (100 hp)
Stall Speed: 69 km/h (both engine options)
Rate of Climb: 4 m/s (80 hp) / 5 m/s (100 hp)
Wing Span: 9.45 m
Length: 6.38 m
Height: 2.20 m
Wing Area: 12.50 m²
Empty Weight: 276 kg (80 hp) / 280 kg (100 hp) Varies with equipment
Max Take-Off Weight (MTOW): 540 kg
Fuel Tank Volume: 65 litres
Payload (approx): 264 kg (80 hp) / 260 kg (100 hp) Depends on interior/equipment
Take-off Distance (grass): up to approx 120 m (80 hp) / 100 m (100 hp)
Glide Ratio: 11 :1
Fuel Consumption (cruise): ~10-13 L/hr
Range (with 65 L tank): approximately 700-750 km (depending on conditions)
Certification Notes: Data state April 2019, technical changes reserved
Shark 600
Engine Option: Rotax 912 ULS (100 hp)
Wing Span: 7.9 m
Length: 6.7 m
Height: 2.5 m
Wing Area: 9.5 m²
Empty Weight (typical): ~295 kg
Max Take-Off Weight (MTOW): 600 kg
Usable Payload (approx.): ~300 kg (pilot, passenger, fuel & baggage)
Fuel Capacity (standard): 100 L
Maximum Cruise Speed (VH): ~300 km/h
Optimum/Economy Cruise Speed: ~250-270 km/h
Stall Speed (clean): ~80 km/h
Stall Speed (flaps down): ~64 km/h
Rate of Climb (at MTOW): ~7.2 m/s
Fuel Consumption (economy): ~15 L/hr
Range (standard fuel): ~1,493 km (subject to configuration)
Load Factor / Structural Limits: +4 g / -2 g (standard version
