Airbus A321-200 vs. Piper PA-34 Seneca

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Airbus A321-200 versus Piper PA-34 Seneca
44.51 m 146 ft 0 in length 8.71 m 28 ft 7 in
11.76 m 38 ft 7 in height 2.99 m 9 ft 10 in
35.8 m 117 ft 5 in wingspan 11.64 m 38 ft 2 in
2 GE CFM56-5B3 engines 2 x Continental IO-360
31,600 lbs thrust per engine 220 lbs
63,200 lbs total thrust 440 lbs
89,000 kg 196,200 lb MTOW 4,750 lb 2,155 kg
4,000 nmi 7,408 km range 980 nm 1,815 km
871 km/h 541 mph cruise speed 165 kts 103 mph
185 to 220 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.