Airbus A310-300 vs. Canadair CT-114 Tutor

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Airbus A310-300 versus Canadair CT-114 Tutor
46.66 m 153 ft 1 in length 9.75 m 32 ft 0 in
15.8 m 51 ft 10 in height 2.84 m 9 ft 4 in
43.9 m 144 ft wingspan 11.07 m 36 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 Orenda J85-CAN-40 turbojet
52,000 lb thrust per engine 2,950 lbs
104,000 lb total thrust 2,950 lbs
148,768 kg 328,000 lb MTOW 3,331 kg 7,350 lb
8,050 km 4,348 nm range 1,520 km 821 nm
482 knots 279 mph cruise speed 310 knots 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.