Grumman OV-1 Mohawk vs. Canadair CL-415

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Grumman OV-1 Mohawk versus Canadair CL-415
12.52 m 41 ft 1 in length 19.82 m 65 ft 0 in
3.89 m 12 ft 9 in height 8.66 m 28 ft 5 in
14.63 m 48 ft wingspan 28.6 m 93 ft 1
2 x Lycoming T53 turboprop engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 1,100 hp each thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 2,200 hp total total thrust 4,300 to 4,760 shaft horsepower
14,950 lb 6,781 kg MTOW 19,733 kg 43,525 lb
1,690 km 913 nm range 1,600 km 864 nm
230 mph 370 km/h cruise speed 290 km/h 180 mph
Pilot and observer capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.