Airbus A220-300 vs. Piper PA-34 Seneca

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Airbus A220-300 versus Piper PA-34 Seneca
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 4,750 lb 2,155 kg
6,297 km 3,402 nm range 980 nm 1,815 km
Mach 0.82 101,3 km/h cruise speed 165 kts 103 mph
Typical seating 2-class 120-150 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.