Avro 652 Anson vs. lockheed C-130 hercules

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Avro 652 Anson versus lockheed C-130 hercules
12.88 m 42 ft 3 in length 29.79 m 97 ft 9 in
2.9 m 9 ft 6 in height 11.66 m 38 ft 3 in
17.22 m 56 ft 6 in wingspan 40.41 m 132 ft 7 in
2 × Armstrong Siddeley Cheetah VI engines 4 x Allison T56-A-15 turboprop engines
290 hp (220 kW) thrust per engine Approximately 4,590 hp per engine
580 hp (440 kW) total thrust Approximately 18,360 hp total
7,500 lb 3,402 kg MTOW 70,307 kg 155,000 lb
1,267 km 684 nm range 3,760 km 2,031 nm
165 mph 266 km/h cruise speed 540 km/h 335 mph
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.