Airbus A310-300 vs. Piper PA-34 Seneca

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Airbus A310-300 versus Piper PA-34 Seneca
46.66 m 153 ft 1 in length 8.71 m 28 ft 7 in
15.8 m 51 ft 10 in height 2.99 m 9 ft 10 in
43.9 m 144 ft wingspan 11.64 m 38 ft 2 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Continental IO-360
52,000 lb thrust per engine 220 lbs
104,000 lb total thrust 440 lbs
148,768 kg 328,000 lb MTOW 4,750 lb 2,155 kg
8,050 km 4,348 nm range 980 nm 1,815 km
482 knots 279 mph cruise speed 165 kts 103 mph
190-230 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.