Airbus A310-300 vs. Praetor 600

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Airbus A310-300 versus Praetor 600
46.66 m 153 ft 1 in length 17.02 m 55 ft 10 in
15.8 m 51 ft 10 in height 6.2 m 20 ft 4 in
43.9 m 144 ft wingspan 20.97 m 68 ft 9 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 Honeywell HTF7500E
52,000 lb thrust per engine 7,036 lbf
104,000 lb total thrust 14,072 lbf
148,768 kg 328,000 lb MTOW 31,750 lb 14,397 kg
8,050 km 4,348 nm range 4,018 nm 7,435 km
482 knots 279 mph cruise speed 466 kts 290 mph
190-230 passengers capacity 12
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.