Airbus A220-100 vs. Beechcraft King Air 260

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Airbus A220-100 versus Beechcraft King Air 260
35.0 m 114 ft 10 in length 13.41 m 43 ft 11 in
11.5 m 37 ft 9 in height 4.57 m 15 ft
35.1 m 115 ft 2 in wingspan 17.39 m 57 ft 1 in
2 Turbofans (wing mounted) engines 2 x Pratt & Whitney Canada PT6A turboprop
21,000–23,000 lb thrust per engine 1050 lbs
42,000–46,000 lb total thrust 2100 lbs
63,100 kg 139,100 lb MTOW 12,500 lb 5,670 kg
6,390 km 3,451 nm range 1,720 nm 3,185 km
871 km/h 541 mph cruise speed 310 kts 193 mph
Typical seating 2-class 100-120 capacity 9
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.