Airbus A321XLR vs. Piper PA-34 Seneca

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Airbus A321XLR 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
CFM LEAP-1A and P&W PW1100G engines 2 x Continental IO-360
33,000 lbs (147 kN) thrust per engine 220 lbs
66,000 lbs (294 kN) total thrust 440 lbs
101,000 kg 222,700 lb MTOW 4,750 lb 2,155 kg
4,700 nmi 8,704 km range 980 nm 1,815 km
963km/h 598mph cruise speed 165 kts 103 mph
180-220 seats (typical 2-class seating) 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.