Airbus A321-200 vs. Canadair CT-114 Tutor
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Airbus A321-200 |
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 |
2 GE CFM56-5B3 |
engines |
1 Orenda J85-CAN-40 turbojet |
31,600 lbs |
thrust per engine |
2,950 lbs |
63,200 lbs |
total thrust |
2,950 lbs |
89,000 kg |
196,200 lb |
MTOW |
3,331 kg |
7,350 lb |
4,000 nmi |
7,408 km |
range |
1,520 km |
821 nm |
871 km/h |
541 mph |
cruise speed |
310 knots |
180 mph |
185 to 220 |
capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.