Airbus A310-300 vs. Fairey Gannet

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Airbus A310-300 versus Fairey Gannet
46.66 m 153 ft 1 in length 10.87 m 35 ft 8 in
15.8 m 51 ft 10 in height 3.76 m 12 ft 4 in
43.9 m 144 ft wingspan 13.87 m 45 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Bristol Pegasus XVIII radial engine
52,000 lb thrust per engine Approximately 690 hp (515 kW)
104,000 lb total thrust Approximately 690 hp (515 kW)
148,768 kg 328,000 lb MTOW 7,005 lb 3,178 kg
8,050 km 4,348 nm range 840 km 454 nm
482 knots 279 mph cruise speed 139 mph 224 km/h
190-230 passengers capacity Pilot, Observer, and Air Gunner
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.