Airbus A300-600 vs. Lockheed Model 18 Lodestar

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Airbus A300-600 versus Lockheed Model 18 Lodestar
54.10 m 177 ft 6 in length 13.61 m 44 ft 8 in
16.5 m 54 ft 2 in height 3.63 m 11 ft 11 in
44.84 m 147 ft 1 in wingspan 19.96 m 65 ft 6 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Wright R-1820 Cyclone radial engines
56,000lb to 61,500lb thrust per engine 1,200 to 1,350 horsepower (895 to 1,007 kW)
112,000–123,000 lb total thrust 2,400 to 2,700 horsepower
171,700 kg 378,600 lb MTOW 9,979 kg 22,000 lb
7,500 km 4,052 nm range 2,500 km 1,350 nm
897 km/h 557 mph cruise speed 300 km/h 186 mph
210-250 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.