Airbus A300-600 vs. Canadair CT-114 Tutor
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Airbus A300-600 |
versus |
Canadair CT-114 Tutor |
54.10 m |
177 ft 6 in |
length |
9.75 m |
32 ft 0 in |
16.5 m |
54 ft 2 in |
height |
2.84 m |
9 ft 4 in |
44.84 m |
147 ft 1 in |
wingspan |
11.07 m |
36 ft 4 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
1 Orenda J85-CAN-40 turbojet |
56,000lb to 61,500lb |
thrust per engine |
2,950 lbs |
112,000–123,000 lb |
total thrust |
2,950 lbs |
171,700 kg |
378,600 lb |
MTOW |
3,331 kg |
7,350 lb |
7,500 km |
4,052 nm |
range |
1,520 km |
821 nm |
897 km/h |
557 mph |
cruise speed |
310 knots |
180 mph |
210-250 passengers |
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.