Airbus A220-100 vs. Bell 206

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Airbus A220-100 versus Bell 206
35.0 m 114 ft 10 in length 12.11 m 39 ft 9 in
11.5 m 37 ft 9 in height 2.88 m 9 ft 5 in
35.1 m 115 ft 2 in wingspan
2 Turbofans (wing mounted) engines 1 × Allison 250-C20B
21,000–23,000 lb thrust per engine 420 shp (313 kW)
42,000–46,000 lb total thrust 420 shp (313 kW)
63,100 kg 139,100 lb MTOW 1,451 kg 3,199 lb
6,390 km 3,451 nm range 374 km 202 nm
871 km/h 541 mph cruise speed 222 km/h 138 mph
Typical seating 2-class 100-120 capacity 1 pilot + 4 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 425 m/min 1,395 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.