Airbus A220-300 vs. Canadair CT-114 Tutor

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Airbus A220-300 versus Canadair CT-114 Tutor
38.7 m 127 ft 0 in length 9.75 m 32 ft 0 in
11.5 m 37 ft 9 in height 2.84 m 9 ft 4 in
35.1 m 115 ft 2 in wingspan 11.07 m 36 ft 4 in
2 x Pratt & Whitney PurePower PW1500G engines 1 Orenda J85-CAN-40 turbojet
21,000–23,000 lb thrust per engine 2,950 lbs
42,000–46,000 lb total thrust 2,950 lbs
70,900 kg 156,300 lb MTOW 3,331 kg 7,350 lb
6,297 km 3,402 nm range 1,520 km 821 nm
Mach 0.82 101,3 km/h cruise speed 310 knots 180 mph
Typical seating 2-class 120-150 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.