Airbus A320-200 vs. Canadair CT-114 Tutor

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Airbus A320-200 versus Canadair CT-114 Tutor
38.7 m 127 ft 0 in length 9.75 m 32 ft 0 in
17.4 m 57 ft 1 in height 2.84 m 9 ft 4 in
35.8 m 117 ft 5 in wingspan 11.07 m 36 ft 4 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 Orenda J85-CAN-40 turbojet
Between 21,000 - 33,000 lbf thrust per engine 2,950 lbs
Between 42,000 - 66,000 lbf total thrust 2,950 lbs
77,000 kg 169,800 lb MTOW 3,331 kg 7,350 lb
5,700 km 3,078 nm range 1,520 km 821 nm
530 mph 853 km/h cruise speed 310 knots 180 mph
Typically between 140-180 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.