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.