Airbus A321XLR vs. McDonnell Douglas A-4 Skyhawk

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Airbus A321XLR versus McDonnell Douglas A-4 Skyhawk
44.51 m 146 ft 0 in length 12.19 m 40 ft 0 in
11.76 m 38 ft 7 in height 4.57 m 15 ft
35.8 m 117 ft 5 in wingspan 8.08 m 26 ft 6 in
CFM LEAP-1A and P&W PW1100G engines 1x Pratt & Whitney J52-P-6A Jet
33,000 lbs (147 kN) thrust per engine 8,500 pound-force
66,000 lbs (294 kN) total thrust 8,500 pound-force
101,000 kg 222,700 lb MTOW 11,113 kg 24,500 lb
4,700 nmi 8,704 km range 3,222 km 1,739 nm
963km/h 598mph cruise speed 586 kts 364 mph
180-220 seats (typical 2-class seating) 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.