Airbus A330-200 vs. Lockheed Ventura

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Airbus A330-200 versus Lockheed Ventura
58.82 m 193 ft 0 in length 15.7 m 51 ft 5 in
17.39 m 57 ft 1 in height 3.6 m 11 ft 10 in
64 m 210 ft wingspan 20 m 65 ft 7 in
2 Turbofans engines 2 x Pratt & Whitney R-2800 radial engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 2,000 hp
Depends on the engine variant total thrust 4,000 hp
251,000 kg 553,400 lb MTOW 15,000 kg 33,100 lb
15,094 km 8,150 nm range 2,670 km 1,440 nmi
531 mph 855 km/h cruise speed 230 mph 370 km/h
220-260 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.