Avro 652 Anson vs. de Havilland Canada DHC-2 Beaver

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Avro 652 Anson versus de Havilland Canada DHC-2 Beaver
12.88 m 42 ft 3 in length 13.56 m 44 ft 6 in
2.9 m 9 ft 6 in height 5 m 16 ft 5 in
17.22 m 56 ft 6 in wingspan 16.56 m 54 ft 4 in
2 × Armstrong Siddeley Cheetah VI engines 2 x Armstrong Siddeley Double Mamba turboprop engines
290 hp (220 kW) thrust per engine Approximately 3,100 hp (2,312 kW) each
580 hp (440 kW) total thrust Approximately 6,200 hp (4,624 kW) total
7,500 lb 3,402 kg MTOW 24,200 lb 10,977 kg
1,267 km 684 nm range 2,535 km 1,369 nm
165 mph 266 km/h cruise speed 228 mph 367 km/h
4 passengers capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.