Airbus A320-200 vs. Lockheed Model 18 Lodestar

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Airbus A320-200 versus Lockheed Model 18 Lodestar
38.7 m 127 ft 0 in length 13.61 m 44 ft 8 in
17.4 m 57 ft 1 in height 3.63 m 11 ft 11 in
35.8 m 117 ft 5 in wingspan 19.96 m 65 ft 6 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Wright R-1820 Cyclone radial engines
Between 21,000 - 33,000 lbf thrust per engine 1,200 to 1,350 horsepower (895 to 1,007 kW)
Between 42,000 - 66,000 lbf total thrust 2,400 to 2,700 horsepower
77,000 kg 169,800 lb MTOW 9,979 kg 22,000 lb
5,700 km 3,078 nm range 2,500 km 1,350 nm
530 mph 853 km/h cruise speed 300 km/h 186 mph
Typically between 140-180 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.