Airbus A330-300 vs. Canadair CL-415
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Airbus A330-300 |
versus |
Canadair CL-415 |
63.66 m |
208 ft 9 in |
length |
19.82 m |
65 ft 0 in |
16.79 m |
55 ft 1 in |
height |
8.66 m |
28 ft 5 in |
60.3 m |
197 ft 9 in |
wingspan |
28.6 m |
93 ft 1 |
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
2 x Pratt & Whitney Canada PW123AF 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 |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
Depends on the engine type |
total thrust |
4,300 to 4,760 shaft horsepower |
242,000 kg |
533,600 lb |
MTOW |
19,733 kg |
43,525 lb |
11,750 km |
6,346 nm |
range |
1,600 km |
864 nm |
900 km/h |
559 mph |
cruise speed |
290 km/h |
180 mph |
250-290 |
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.