Airbus A220-100 vs. Bell 412

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Airbus A220-100 versus Bell 412
35.0 m 114 ft 10 in length 17,10 m 56 ft 1 in
11.5 m 37 ft 9 in height 3,48 m 11 ft 5 in
35.1 m 115 ft 2 in wingspan
2 Turbofans (wing mounted) engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
21,000–23,000 lb thrust per engine 1,800 hp
42,000–46,000 lb total thrust 3,600 hp
63,100 kg 139,100 lb MTOW 5,400 kg 11,905 lb
6,390 km 3,451 nm range 659 km 356 nm
871 km/h 541 mph cruise speed 259 km/h 161 mph
Typical seating 2-class 100-120 capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.