Avro 652 Anson vs. Lockheed P-2 Neptune

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Avro 652 Anson versus Lockheed P-2 Neptune
12.88 m 42 ft 3 in length 30.17 m 99 ft 0 in
2.9 m 9 ft 6 in height 10.15 m 33 ft 4 in
17.22 m 56 ft 6 in wingspan 33.53 m 110 ft
2 × Armstrong Siddeley Cheetah VI engines 2 x Wright R-3350 radial engines
290 hp (220 kW) thrust per engine Approximately 3,700 hp
580 hp (440 kW) total thrust Approximately 7,400 hp
7,500 lb 3,402 kg MTOW 27,216 kg 60,000 lb
1,267 km 684 nm range 7,885 km 4,259 nm
165 mph 266 km/h cruise speed 300 mph 483 km/h
4 passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.