Airbus A310-300 vs. Piper PA-46

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Airbus A310-300 versus Piper PA-46
46.66 m 153 ft 1 in length 8.71 m 28 ft 7 in
15.8 m 51 ft 10 in height 3.45 m 11 ft 4 in
43.9 m 144 ft wingspan 13.11 m 43 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Lycoming TIO-540
52,000 lb thrust per engine 350 lbs
104,000 lb total thrust 350 lbs
148,768 kg 328,000 lb MTOW 4,100 lb 1,860 kg
8,050 km 4,348 nm range 1410 nm 2,611 km
482 knots 279 mph cruise speed 214 kts 133 mph
190-230 passengers capacity 6
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.