Airbus A300-600 vs. de Havilland DH-82 Tiger Moth

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Airbus A300-600 versus de Havilland DH-82 Tiger Moth
54.10 m 177 ft 6 in length 7.29 m 23 ft 11 in
16.5 m 54 ft 2 in height 2.67 m 8 ft 9 in
44.84 m 147 ft 1 in wingspan 8.97 m 29 ft 5 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 x de Havilland Gipsy Major I inline engine
56,000lb to 61,500lb thrust per engine Approximately 130 hp
112,000–123,000 lb total thrust Approximately 130 hp
171,700 kg 378,600 lb MTOW 1,825 lb 828 kg
7,500 km 4,052 nm range 322 km 174 nm
897 km/h 557 mph cruise speed 78 mph 126 km/h
210-250 passengers capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.