Airbus A310-300 vs. Air Tractor AT-802

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Airbus A310-300 versus Air Tractor AT-802
46.66 m 153 ft 1 in length 10.16 m 33 ft 4 in
15.8 m 51 ft 10 in height 3.66 m 12 ft
43.9 m 144 ft wingspan 18.29 m 60 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Pratt & Whitney Canada PT6A-67F turboprop engine
52,000 lb thrust per engine 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
104,000 lb total thrust 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
148,768 kg 328,000 lb MTOW 7,257 kg 16,000 lb
8,050 km 4,348 nm range 1,125 km 607 nm
482 knots 279 mph cruise speed 240 km/h 149 mph
190-230 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.