Airbus A220-100 vs. Canadair CT-114 Tutor

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Airbus A220-100 versus Canadair CT-114 Tutor
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 3,331 kg 7,350 lb
6,390 km 3,451 nm range 1,520 km 821 nm
871 km/h 541 mph cruise speed 310 knots 180 mph
Typical seating 2-class 100-120 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.