Academically, here are the general specs of these aircrafts:
Eurocopter Fennec
Eurocopter Fennec - Wikipedia, the free encyclopedia
General characteristics
Crew: 2
Capacity: 4 passengers
Length: 10.93 m (35 ft 10 in) (fuselage length), 12.94 m (42 ft 6 in) (overall length, rotors turning)
Height: 3.34 m (10 ft 11 in)
Empty weight: 1,220 kg (2,690 lb)
Max takeoff weight: 2,250 kg (4,960 lb)
Fuel capacity: 540 L (143 US Gal)
Powerplant: 1 × Turbomeca Arriel 2B turboshaft, 632 kW (847 shp) (limited to 500 kW (671 shp for take-off)
Main rotor diameter: 10.69 m (35 ft 1 in)
Main rotor area: 89.75 m2 (966.1 sq ft)
Performance
Maximum speed: 246 km/h (153 mph; 133 kn) (max cruise)
Never exceed speed: 287 km/h (178 mph; 155 kn)
Range: 648 km (403 mi; 350 nmi)
Service ceiling: 5,280 m (17,323 ft)
Rate of climb: 10.30 m/s (2,028 ft/min)
Kamov Ka-226
Kamov Ka-226 - Wikipedia, the free encyclopedia
General characteristics
Crew: 1
Passengers: 9
Cargo: 1,400kg internally, or 1,500kg on an external sling
Length: 8.1 m (25 ft 7 in)
Main rotor diameter: 2× 13 m (42 ft 8 in)
Height: 4.15 m (13 ft 7 in)
Gross weight: 3400 kg (7496 lb)
Powerplant: 2 × Turbomeca Arrius 2G1, 335 kW (450 hp) each
Performance
Maximum speed: 205 km/h (127 mph)
Cruising speed: 195 km/h (121 mph)
Range: 600 km (372 miles)
Service ceiling: 6200 m (20300 ft) -
This is increased to as much as 7000 m with the Turbomeca Arrius engine
Hover ceiling: 2500 m (8200 ft)