Cessna O-2 Skymaster vs. Grumman OV-1 Mohawk

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Cessna O-2 Skymaster versus Grumman OV-1 Mohawk
8.9 m 29 ft 2 in length 12.52 m 41 ft 1 in
2.87 m 9 ft 5 in height 3.89 m 12 ft 9 in
11.58 m 38 ft wingspan 14.63 m 48 ft
Two 210-hp Continental IO-360s engines 2 x Lycoming T53 turboprop engines
210 hp thrust per engine Approximately 1,100 hp each
420 hp total thrust Approximately 2,200 hp total
5,400 lb 2,449 kg MTOW 14,950 lb 6,781 kg
1,705 km 921 nm range 1,690 km 913 nm
144 mph 232 km/h cruise speed 230 mph 370 km/h
2 capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.