Avro 652 Anson vs. Grumman OV-1 Mohawk

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Avro 652 Anson versus Grumman OV-1 Mohawk
12.88 m 42 ft 3 in length 12.52 m 41 ft 1 in
2.9 m 9 ft 6 in height 3.89 m 12 ft 9 in
17.22 m 56 ft 6 in wingspan 14.63 m 48 ft
2 × Armstrong Siddeley Cheetah VI engines 2 x Lycoming T53 turboprop engines
290 hp (220 kW) thrust per engine Approximately 1,100 hp each
580 hp (440 kW) total thrust Approximately 2,200 hp total
7,500 lb 3,402 kg MTOW 14,950 lb 6,781 kg
1,267 km 684 nm range 1,690 km 913 nm
165 mph 266 km/h cruise speed 230 mph 370 km/h
4 passengers 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.