Airbus A310-300 vs. de Havilland DH-82 Tiger Moth

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Airbus A310-300 versus de Havilland DH-82 Tiger Moth
46.66 m 153 ft 1 in length 7.29 m 23 ft 11 in
15.8 m 51 ft 10 in height 2.67 m 8 ft 9 in
43.9 m 144 ft wingspan 8.97 m 29 ft 5 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x de Havilland Gipsy Major I inline engine
52,000 lb thrust per engine Approximately 130 hp
104,000 lb total thrust Approximately 130 hp
148,768 kg 328,000 lb MTOW 1,825 lb 828 kg
8,050 km 4,348 nm range 322 km 174 nm
482 knots 279 mph cruise speed 78 mph 126 km/h
190-230 passengers capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.