Airbus A340-200 vs. Mitsubishi A6M Zero

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Airbus A340-200 versus Mitsubishi A6M Zero
59.4 m 194 ft 11 in length 9.06 m 29 ft 9 in
16.8 m 55 ft 1 in height 3.05 m 10 ft
60.3 m 197 ft 9 in wingspan 12 m 39 ft 4 in
4 x CFM International CFM56-5C4 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
34,000 lbf thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
136,000 lbf total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
275,000 kg 606,300 lb MTOW 2,800 kg 6,170 lb
12,400 km 6,699 nm range 1,010 nm 1,871 km
880 km/h 547 mph cruise speed 180 knots 105 mph
Typical seating 3-class 210-250 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.