North American Rockwell OV-10 Bronco vs. Canadair CL-415
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| North American Rockwell OV-10 Bronco |
versus |
Canadair CL-415 |
| 12.7 m |
41 ft 7 in |
length |
19.82 m |
65 ft 0 in |
| 4.62 m |
15 ft 2 in |
height |
8.66 m |
28 ft 5 in |
| 12.19 m |
40 ft |
wingspan |
28.6 m |
93 ft 1 |
| 2 x Garrett T76-G-420/421 turboprop engines |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
| Approximately 715 hp each |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
| Approximately 1,430 hp total |
total thrust |
4,300 to 4,760 shaft horsepower |
| 14,444 lb |
6,553 kg |
MTOW |
19,733 kg |
43,525 lb |
| 1,931 km |
1,043 nm |
range |
1,600 km |
864 nm |
| 244 mph |
393 km/h |
cruise speed |
290 km/h |
180 mph |
| Pilot and observer |
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.
