Airbus A220-100 vs. Piper PA-34 Seneca

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Airbus A220-100 versus Piper PA-34 Seneca
35.0 m 114 ft 10 in length 8.71 m 28 ft 7 in
11.5 m 37 ft 9 in height 2.99 m 9 ft 10 in
35.1 m 115 ft 2 in wingspan 11.64 m 38 ft 2 in
2 Turbofans (wing mounted) engines 2 x Continental IO-360
21,000–23,000 lb thrust per engine 220 lbs
42,000–46,000 lb total thrust 440 lbs
63,100 kg 139,100 lb MTOW 4,750 lb 2,155 kg
6,390 km 3,451 nm range 980 nm 1,815 km
871 km/h 541 mph cruise speed 165 kts 103 mph
Typical seating 2-class 100-120 capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.