Airbus A220-100 vs. Piper PA-46

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Airbus A220-100 versus Piper PA-46
35.0 m 114 ft 10 in length 8.71 m 28 ft 7 in
11.5 m 37 ft 9 in height 3.45 m 11 ft 4 in
35.1 m 115 ft 2 in wingspan 13.11 m 43 ft
2 Turbofans (wing mounted) engines 1 x Lycoming TIO-540
21,000–23,000 lb thrust per engine 350 lbs
42,000–46,000 lb total thrust 350 lbs
63,100 kg 139,100 lb MTOW 4,100 lb 1,860 kg
6,390 km 3,451 nm range 1410 nm 2,611 km
871 km/h 541 mph cruise speed 214 kts 133 mph
Typical seating 2-class 100-120 capacity 6
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.