Canadair CT-114 Tutor vs. Airbus H225 Super Puma

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Canadair CT-114 Tutor versus Airbus H225 Super Puma
9.75 m 32 ft 0 in length 14.06 m 46 ft 2 in
2.84 m 9 ft 4 in height 4.38 m 14 ft 4 in
11.07 m 36 ft 4 in wingspan
1 Orenda J85-CAN-40 turbojet engines 2 x Turbomeca Makila 2A turboshaft engines
2,950 lbs thrust per engine 2,778 hp
2,950 lbs total thrust 5,556 hp
3,331 kg 7,350 lb MTOW 11,000 kg 24,251 lb
1,520 km 821 nm range 857 km 463 nm
310 knots 180 mph cruise speed 242 km/h 150 mph
capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.