Airbus A220-100 vs. Mitsubishi A6M Zero

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Airbus A220-100 versus Mitsubishi A6M Zero
35.0 m 114 ft 10 in length 9.06 m 29 ft 9 in
11.5 m 37 ft 9 in height 3.05 m 10 ft
35.1 m 115 ft 2 in wingspan 12 m 39 ft 4 in
2 Turbofans (wing mounted) engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
21,000–23,000 lb thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
42,000–46,000 lb total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
63,100 kg 139,100 lb MTOW 2,800 kg 6,170 lb
6,390 km 3,451 nm range 1,010 nm 1,871 km
871 km/h 541 mph cruise speed 180 knots 105 mph
Typical seating 2-class 100-120 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.