Canadair CL-415 vs. Piper PA-34 Seneca
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Canadair CL-415 |
versus |
Piper PA-34 Seneca |
19.82 m |
65 ft 0 in |
length |
8.71 m |
28 ft 7 in |
8.66 m |
28 ft 5 in |
height |
2.99 m |
9 ft 10 in |
28.6 m |
93 ft 1 |
wingspan |
11.64 m |
38 ft 2 in |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
engines |
2 x Continental IO-360 |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
thrust per engine |
220 lbs |
4,300 to 4,760 shaft horsepower |
total thrust |
440 lbs |
19,733 kg |
43,525 lb |
MTOW |
4,750 lb |
2,155 kg |
1,600 km |
864 nm |
range |
980 nm |
1,815 km |
290 km/h |
180 mph |
cruise speed |
165 kts |
103 mph |
|
capacity |
5 |
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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.