Airbus A310-300 vs. Beechcraft T-34 Mentor

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Airbus A310-300 versus Beechcraft T-34 Mentor
46.66 m 153 ft 1 in length 7.92 m 25 ft 11 in
15.8 m 51 ft 10 in height 2.95 m 9 ft 8 in
43.9 m 144 ft wingspan 10.03 m 32 ft 11 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Continental Motors IO-520 engine
52,000 lb thrust per engine Approximately 300 hp
104,000 lb total thrust Approximately 300 hp
148,768 kg 328,000 lb MTOW 3,100 lb 1,406 kg
8,050 km 4,348 nm range 1,111 km 600 nm
482 knots 279 mph cruise speed 190 mph 306 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.