Bombardier CRJ1000 vs. de Havilland Canada DHC-6 Twin Otter
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here.
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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.