Airbus A330-200 vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A330-200 versus de Havilland Canada DHC-6 Twin Otter
58.82 m 193 ft 0 in length 15.32 m 50 ft 3 in
17.39 m 57 ft 1 in height 5.94 m 19 ft 6 in
64 m 210 ft wingspan 19.81 m 65 ft
2 Turbofans engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
Depends on the engine variant total thrust 1100 to 1500 shaft horsepower
251,000 kg 553,400 lb MTOW 5,670 kg 12,500 lb
15,094 km 8,150 nm range 1,389 km 750 nm
531 mph 855 km/h cruise speed 280 km/h 174 mph
220-260 capacity 19 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.