Airbus A310-300 vs. Fairchild PT-19 Cornell

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Airbus A310-300 versus Fairchild PT-19 Cornell
46.66 m 153 ft 1 in length 8.79 m 28 ft 10 in
15.8 m 51 ft 10 in height 2.26 m 7 ft 5 in
43.9 m 144 ft wingspan 10.97 m 36 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Ranger L-440-5 inline engine
52,000 lb thrust per engine Approximately 175 hp
104,000 lb total thrust Approximately 175 hp
148,768 kg 328,000 lb MTOW 2,450 lb 1,111 kg
8,050 km 4,348 nm range 660 km 356 nm
482 knots 279 mph cruise speed 125 mph 201 km/h
190-230 passengers capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.