Boeing 717-200HGW vs. Mitsubishi A6M Zero

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Boeing 717-200HGW versus Mitsubishi A6M Zero
37.80 m 123 ft 11 in length 9.06 m 29 ft 9 in
8.87 m 29 ft 1 in height 3.05 m 10 ft
28.44 m 93 ft 4 in wingspan 12 m 39 ft 4 in
2 Rolls-Royce BR715 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
82.3kN (18,500lb) to 93.4kN (21,000lb) thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
164.6kN (37,000lb) to 186.8kN (42,000lb) total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
54,885 kg 121,000 lb MTOW 2,800 kg 6,170 lb
2,060 nm 3,814 km range 1,010 nm 1,871 km
811 km/h 504 mph cruise speed 180 knots 105 mph
106 passengers in a 2 class configuration 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.