Avro 652 Anson vs. Polikarpov I-16

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Avro 652 Anson versus Polikarpov I-16
12.88 m 42 ft 3 in length 6.13 m 20 ft 1 in
2.9 m 9 ft 6 in height 3.25 m 10 ft 8 in
17.22 m 56 ft 6 in wingspan 9 m 29 ft 6 in
2 × Armstrong Siddeley Cheetah VI engines 1x Shvetsov M-25 radial engine
290 hp (220 kW) thrust per engine 1000 hp
580 hp (440 kW) total thrust 1000 hp
7,500 lb 3,402 kg MTOW 2,060 kg 4,540 lb
1,267 km 684 nm range 248 mi 216 nm
165 mph 266 km/h cruise speed 180 mph 290 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.