Airbus A220-100 vs. McDonnell Douglas A-4 Skyhawk

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Airbus A220-100 versus McDonnell Douglas A-4 Skyhawk
35.0 m 114 ft 10 in length 12.19 m 40 ft 0 in
11.5 m 37 ft 9 in height 4.57 m 15 ft
35.1 m 115 ft 2 in wingspan 8.08 m 26 ft 6 in
2 Turbofans (wing mounted) engines 1x Pratt & Whitney J52-P-6A Jet
21,000–23,000 lb thrust per engine 8,500 pound-force
42,000–46,000 lb total thrust 8,500 pound-force
63,100 kg 139,100 lb MTOW 11,113 kg 24,500 lb
6,390 km 3,451 nm range 3,222 km 1,739 nm
871 km/h 541 mph cruise speed 586 kts 364 mph
Typical seating 2-class 100-120 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.