Airbus A310-300 vs. McDonnell Douglas A-4 Skyhawk

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Airbus A310-300 versus McDonnell Douglas A-4 Skyhawk
46.66 m 153 ft 1 in length 12.19 m 40 ft 0 in
15.8 m 51 ft 10 in height 4.57 m 15 ft
43.9 m 144 ft wingspan 8.08 m 26 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1x Pratt & Whitney J52-P-6A Jet
52,000 lb thrust per engine 8,500 pound-force
104,000 lb total thrust 8,500 pound-force
148,768 kg 328,000 lb MTOW 11,113 kg 24,500 lb
8,050 km 4,348 nm range 3,222 km 1,739 nm
482 knots 279 mph cruise speed 586 kts 364 mph
190-230 passengers capacity Up to 9,155 pounds of weapons on 5 hardpoints
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.