Airbus A340-600 vs. Canadair CL-415
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Airbus A340-600 |
versus |
Canadair CL-415 |
75.36 m |
247 ft 3 in |
length |
19.82 m |
65 ft 0 in |
17.93 m |
58 ft 10 in |
height |
8.66 m |
28 ft 5 in |
63.45 m |
208 ft 2 in |
wingspan |
28.6 m |
93 ft 1 |
4 x Rolls-Royce Trent 556 |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
56,000 lbs |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
224,000 lbs |
total thrust |
4,300 to 4,760 shaft horsepower |
380,000 kg |
837,800 lb |
MTOW |
19,733 kg |
43,525 lb |
14,450 km |
7,804 nm |
range |
1,600 km |
864 nm |
890 km/h |
553 mph |
cruise speed |
290 km/h |
180 mph |
320-370 |
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.