Airbus A310-300 vs. Canadair CL-415

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Airbus A310-300 versus Canadair CL-415
46.66 m 153 ft 1 in length 19.82 m 65 ft 0 in
15.8 m 51 ft 10 in height 8.66 m 28 ft 5 in
43.9 m 144 ft wingspan 28.6 m 93 ft 1
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
52,000 lb thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
104,000 lb total thrust 4,300 to 4,760 shaft horsepower
148,768 kg 328,000 lb MTOW 19,733 kg 43,525 lb
8,050 km 4,348 nm range 1,600 km 864 nm
482 knots 279 mph cruise speed 290 km/h 180 mph
190-230 passengers 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.