Canadair CT-114 Tutor vs. Percival Provost

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Canadair CT-114 Tutor versus Percival Provost
9.75 m 32 ft 0 in length 9.0 m 29 ft 6 in
2.84 m 9 ft 4 in height 3.02 m 9 ft 11 in
11.07 m 36 ft 4 in wingspan 12.19 m 40 ft
1 Orenda J85-CAN-40 turbojet engines 1 x Alvis Leonides Major 755/1 inline engine
2,950 lbs thrust per engine Approximately 550 hp
2,950 lbs total thrust Approximately 550 hp
3,331 kg 7,350 lb MTOW 5,500 lb 2,495 kg
1,520 km 821 nm range 1,127 km 608 nm
310 knots 180 mph cruise speed 175 mph 282 km/h
capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.