Airbus A220-100 vs. Lockheed Ventura

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Airbus A220-100 versus Lockheed Ventura
35.0 m 114 ft 10 in length 15.7 m 51 ft 5 in
11.5 m 37 ft 9 in height 3.6 m 11 ft 10 in
35.1 m 115 ft 2 in wingspan 20 m 65 ft 7 in
2 Turbofans (wing mounted) engines 2 x Pratt & Whitney R-2800 radial engines
21,000–23,000 lb thrust per engine 2,000 hp
42,000–46,000 lb total thrust 4,000 hp
63,100 kg 139,100 lb MTOW 15,000 kg 33,100 lb
6,390 km 3,451 nm range 2,670 km 1,440 nmi
871 km/h 541 mph cruise speed 230 mph 370 km/h
Typical seating 2-class 100-120 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.