Cessna O-2 Skymaster vs. Canadair CL-415
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Cessna O-2 Skymaster |
versus |
Canadair CL-415 |
8.9 m |
29 ft 2 in |
length |
19.82 m |
65 ft 0 in |
2.87 m |
9 ft 5 in |
height |
8.66 m |
28 ft 5 in |
11.58 m |
38 ft |
wingspan |
28.6 m |
93 ft 1 |
Two 210-hp Continental IO-360s |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
210 hp |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
420 hp |
total thrust |
4,300 to 4,760 shaft horsepower |
5,400 lb |
2,449 kg |
MTOW |
19,733 kg |
43,525 lb |
1,705 km |
921 nm |
range |
1,600 km |
864 nm |
144 mph |
232 km/h |
cruise speed |
290 km/h |
180 mph |
2 |
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.