Airbus A310-300 vs. Lockheed Ventura

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Airbus A310-300 versus Lockheed Ventura
46.66 m 153 ft 1 in length 15.7 m 51 ft 5 in
15.8 m 51 ft 10 in height 3.6 m 11 ft 10 in
43.9 m 144 ft wingspan 20 m 65 ft 7 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Pratt & Whitney R-2800 radial engines
52,000 lb thrust per engine 2,000 hp
104,000 lb total thrust 4,000 hp
148,768 kg 328,000 lb MTOW 15,000 kg 33,100 lb
8,050 km 4,348 nm range 2,670 km 1,440 nmi
482 knots 279 mph cruise speed 230 mph 370 km/h
190-230 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.