Airbus A340-500 vs. Mitsubishi A6M Zero

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Airbus A340-500 versus Mitsubishi A6M Zero
67.93 m 222 ft 10 in length 9.06 m 29 ft 9 in
17.53 m 57 ft 6 in height 3.05 m 10 ft
63.45 m 208 ft 2 in wingspan 12 m 39 ft 4 in
4 Rolls-Royce Trent 500 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
54,000 lbf (240 kN) thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
216,000 lbf (960 kN) total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
380,000 kg 837,800 lb MTOW 2,800 kg 6,170 lb
16,670 km 9,000 nm range 1,010 nm 1,871 km
475 knots 880 km/h cruise speed 180 knots 105 mph
Typical seating 3-class 270-310 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.