Airbus A310-300 vs. Cessna 172

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Airbus A310-300 versus Cessna 172
46.66 m 153 ft 1 in length 8.28 m 27 ft 2 in
15.8 m 51 ft 10 in height 2.72 m 8 ft 11 in
43.9 m 144 ft wingspan 11 m 36 ft 1 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Lycoming IO-360-L2A flat-4 piston engine
52,000 lb thrust per engine 180 to 200 horsepower (134 to 149 kW)
104,000 lb total thrust 180 to 200 horsepower (134 to 149 kW)
148,768 kg 328,000 lb MTOW 1,040 kg 2,293 lb
8,050 km 4,348 nm range 1,056 km 570 nm
482 knots 279 mph cruise speed 226 km/h 140 mph
190-230 passengers capacity 4
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.