Bombardier CRJ1000 vs. de Havilland Canada DHC-6 Twin Otter

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Bombardier CRJ1000 versus de Havilland Canada DHC-6 Twin Otter
39.1 m 128 ft 5 in length 15.32 m 50 ft 3 in
7.5 m 24 ft 7 in height 5.94 m 19 ft 6 in
26.2 m 86 ft wingspan 19.81 m 65 ft
2 GE CF34-8C5A1 turbofans engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 1100 to 1500 shaft horsepower
41,640 kg 91,800 lb MTOW 5,670 kg 12,500 lb
3,004 km 1,623 nm range 1,389 km 750 nm
515 mph 829 km/h cruise speed 280 km/h 174 mph
100 (common) 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.