Airbus A330-300 vs. de Havilland Canada DHC-6 Twin Otter
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here.
| Airbus A330-300 |
versus |
de Havilland Canada DHC-6 Twin Otter |
| 63.66 m |
208 ft 9 in |
length |
15.32 m |
50 ft 3 in |
| 16.79 m |
55 ft 1 in |
height |
5.94 m |
19 ft 6 in |
| 60.3 m |
197 ft 9 in |
wingspan |
19.81 m |
65 ft |
| General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
| 311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
| Depends on the engine type |
total thrust |
1100 to 1500 shaft horsepower |
| 242,000 kg |
533,600 lb |
MTOW |
5,670 kg |
12,500 lb |
| 11,750 km |
6,346 nm |
range |
1,389 km |
750 nm |
| 900 km/h |
559 mph |
cruise speed |
280 km/h |
174 mph |
| 250-290 |
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.
