Airbus A300-600 vs. Lockheed Ventura

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Airbus A300-600 versus Lockheed Ventura
54.10 m 177 ft 6 in length 15.7 m 51 ft 5 in
16.5 m 54 ft 2 in height 3.6 m 11 ft 10 in
44.84 m 147 ft 1 in wingspan 20 m 65 ft 7 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Pratt & Whitney R-2800 radial engines
56,000lb to 61,500lb thrust per engine 2,000 hp
112,000–123,000 lb total thrust 4,000 hp
171,700 kg 378,600 lb MTOW 15,000 kg 33,100 lb
7,500 km 4,052 nm range 2,670 km 1,440 nmi
897 km/h 557 mph cruise speed 230 mph 370 km/h
210-250 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.