Avro 652 Anson vs. Lockheed Ventura

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Avro 652 Anson versus Lockheed Ventura
12.88 m 42 ft 3 in length 15.7 m 51 ft 5 in
2.9 m 9 ft 6 in height 3.6 m 11 ft 10 in
17.22 m 56 ft 6 in wingspan 20 m 65 ft 7 in
2 × Armstrong Siddeley Cheetah VI engines 2 x Pratt & Whitney R-2800 radial engines
290 hp (220 kW) thrust per engine 2,000 hp
580 hp (440 kW) total thrust 4,000 hp
7,500 lb 3,402 kg MTOW 15,000 kg 33,100 lb
1,267 km 684 nm range 2,670 km 1,440 nmi
165 mph 266 km/h cruise speed 230 mph 370 km/h
4 passengers 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.