Airbus A310-300 vs. Lockheed Model 18 Lodestar

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Airbus A310-300 versus Lockheed Model 18 Lodestar
46.66 m 153 ft 1 in length 13.61 m 44 ft 8 in
15.8 m 51 ft 10 in height 3.63 m 11 ft 11 in
43.9 m 144 ft wingspan 19.96 m 65 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Wright R-1820 Cyclone radial engines
52,000 lb thrust per engine 1,200 to 1,350 horsepower (895 to 1,007 kW)
104,000 lb total thrust 2,400 to 2,700 horsepower
148,768 kg 328,000 lb MTOW 9,979 kg 22,000 lb
8,050 km 4,348 nm range 2,500 km 1,350 nm
482 knots 279 mph cruise speed 300 km/h 186 mph
190-230 passengers capacity 14 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.