Airbus A220-300 vs. Bell 206

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Airbus A220-300 versus Bell 206
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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)
70,900 kg 156,300 lb MTOW 1,451 kg 3,199 lb
6,297 km 3,402 nm range 374 km 202 nm
Mach 0.82 101,3 km/h cruise speed 222 km/h 138 mph
Typical seating 2-class 120-150 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.