Airbus A310-300 vs. Westland Lysander

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Airbus A310-300 versus Westland Lysander
46.66 m 153 ft 1 in length 9.3 m 30 ft 6 in
15.8 m 51 ft 10 in height 3.51 m 11 ft 6 in
43.9 m 144 ft wingspan 15.24 m 50 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Bristol Mercury XII radial engine
52,000 lb thrust per engine Approximately 870 hp
104,000 lb total thrust Approximately 870 hp
148,768 kg 328,000 lb MTOW 7,500 lb 3,402 kg
8,050 km 4,348 nm range 966 km 522 nm
482 knots 279 mph cruise speed 190 mph 306 km/h
190-230 passengers capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.