Airbus A310-300 vs. de Havilland Canada DHC-3 Otter
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Airbus A310-300 |
versus |
de Havilland Canada DHC-3 Otter |
46.66 m |
153 ft 1 in |
length |
10.52 m |
34 ft 6 in |
15.8 m |
51 ft 10 in |
height |
3.84 m |
12 ft 7 in |
43.9 m |
144 ft |
wingspan |
17.68 m |
58 ft |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
1 x Pratt & Whitney R-1340 radial engine |
52,000 lb |
thrust per engine |
400 to 600 horsepower (298 to 447 kW) |
104,000 lb |
total thrust |
400 to 600 horsepower (298 to 447 kW) |
148,768 kg |
328,000 lb |
MTOW |
5,670 kg |
12,500 lb |
8,050 km |
4,348 nm |
range |
1,296 km |
700 nm |
482 knots |
279 mph |
cruise speed |
215 km/h |
134 mph |
190-230 passengers |
capacity |
10-11 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.