Airbus A321LR vs. Canadair CT-114 Tutor

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Airbus A321LR versus Canadair CT-114 Tutor
44.51 m 146 ft 0 in length 9.75 m 32 ft 0 in
11.76 m 38 ft 7 in height 2.84 m 9 ft 4 in
35.8 m 117 ft 5 in wingspan 11.07 m 36 ft 4 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 Orenda J85-CAN-40 turbojet
Over 33,000 lbs (147 kN) thrust per engine 2,950 lbs
66,000 lbs (294 kN) total thrust 2,950 lbs
97,000 kg 213,800 lb MTOW 3,331 kg 7,350 lb
7,400 km 4,000 nm range 1,520 km 821 nm
832 km/h 517 mph cruise speed 310 knots 180 mph
180-220 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.