Boeing 747-400 vs. Mitsubishi A6M Zero

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Boeing 747-400 versus Mitsubishi A6M Zero
70.56 m 231 ft 10 in length 9.06 m 29 ft 9 in
19.3 m 63 ft 4 in height 3.05 m 10 ft
59.49 m 195 ft 4 in wingspan 12 m 39 ft 4 in
Pratt & Whitney PW4000, General Electric CF6 -80C2 or Rolls-Royce RB211 -524G/H engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
Around 60,000 to 70,000 pounds thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Around 240,000 to 280,000 pounds total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
396,834 kg 875,000 lb MTOW 2,800 kg 6,170 lb
13,492 km 7,285 nmi range 1,010 nm 1,871 km
939 km/h 584 mph cruise speed 180 knots 105 mph
Typically accommodates 416 passengers in a three-class layout 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.