Airbus A330-200 vs. Canadair CL-415
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Airbus A330-200 |
versus |
Canadair CL-415 |
58.82 m |
193 ft 0 in |
length |
19.82 m |
65 ft 0 in |
17.39 m |
57 ft 1 in |
height |
8.66 m |
28 ft 5 in |
64 m |
210 ft |
wingspan |
28.6 m |
93 ft 1 |
2 Turbofans |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
Depends on the engine variant |
total thrust |
4,300 to 4,760 shaft horsepower |
251,000 kg |
553,400 lb |
MTOW |
19,733 kg |
43,525 lb |
15,094 km |
8,150 nm |
range |
1,600 km |
864 nm |
531 mph |
855 km/h |
cruise speed |
290 km/h |
180 mph |
220-260 |
capacity |
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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.