Airbus A320-200 vs. Piper PA-34 Seneca

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Airbus A320-200 versus Piper PA-34 Seneca
38.7 m 127 ft 0 in length 8.71 m 28 ft 7 in
17.4 m 57 ft 1 in height 2.99 m 9 ft 10 in
35.8 m 117 ft 5 in wingspan 11.64 m 38 ft 2 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Continental IO-360
Between 21,000 - 33,000 lbf thrust per engine 220 lbs
Between 42,000 - 66,000 lbf total thrust 440 lbs
77,000 kg 169,800 lb MTOW 4,750 lb 2,155 kg
5,700 km 3,078 nm range 980 nm 1,815 km
530 mph 853 km/h cruise speed 165 kts 103 mph
Typically between 140-180 passengers 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.