Airbus A319neo vs. de Havilland Canada DHC-6 Twin Otter
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Airbus A319neo |
versus |
de Havilland Canada DHC-6 Twin Otter |
33.84 m |
111 ft 0 in |
length |
15.32 m |
50 ft 3 in |
11.76 m |
38 ft 7 in |
height |
5.94 m |
19 ft 6 in |
35.8 m |
117 ft 5 in |
wingspan |
19.81 m |
65 ft |
2 x PW 1100G or 2 x CFM LEAP-1A |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) |
total thrust |
1100 to 1500 shaft horsepower |
75,500 kg |
166,400 lb |
MTOW |
5,670 kg |
12,500 lb |
6,850 km |
3,702 nm |
range |
1,389 km |
750 nm |
530 mph |
853 km/h |
cruise speed |
280 km/h |
174 mph |
120-150 |
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.