Airbus A310-300 vs. Beechcraft T-6 Texan II

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Airbus A310-300 versus Beechcraft T-6 Texan II
46.66 m 153 ft 1 in length 10.18 m 33 ft 4 in
15.8 m 51 ft 10 in height 3.29 m 10 ft 10 in
43.9 m 144 ft wingspan 10.21 m 33 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Pratt & Whitney Canada PT6A-68
52,000 lb thrust per engine 1100 lbs
104,000 lb total thrust 1100 lbs
148,768 kg 328,000 lb MTOW 6,250 lb 2,835 kg
8,050 km 4,348 nm range 900 nm 1,667 km
482 knots 279 mph cruise speed 320 kts 199 mph
190-230 passengers capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.