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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.