Airbus A300-600 vs. de Havilland Canada DHC-6 Twin Otter
... or view the full comparison list
here.
Airbus A300-600 |
versus |
de Havilland Canada DHC-6 Twin Otter |
54.10 m |
177 ft 6 in |
length |
15.32 m |
50 ft 3 in |
16.5 m |
54 ft 2 in |
height |
5.94 m |
19 ft 6 in |
44.84 m |
147 ft 1 in |
wingspan |
19.81 m |
65 ft |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
56,000lb to 61,500lb |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
112,000–123,000 lb |
total thrust |
1100 to 1500 shaft horsepower |
171,700 kg |
378,600 lb |
MTOW |
5,670 kg |
12,500 lb |
7,500 km |
4,052 nm |
range |
1,389 km |
750 nm |
897 km/h |
557 mph |
cruise speed |
280 km/h |
174 mph |
210-250 passengers |
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.