Airbus A300-600 vs. Bell 206

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Airbus A300-600 versus Bell 206
54.10 m 177 ft 6 in length 12.11 m 39 ft 9 in
16.5 m 54 ft 2 in height 2.88 m 9 ft 5 in
44.84 m 147 ft 1 in wingspan
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 × Allison 250-C20B
56,000lb to 61,500lb thrust per engine 420 shp (313 kW)
112,000–123,000 lb total thrust 420 shp (313 kW)
171,700 kg 378,600 lb MTOW 1,451 kg 3,199 lb
7,500 km 4,052 nm range 374 km 202 nm
897 km/h 557 mph cruise speed 222 km/h 138 mph
210-250 passengers capacity 1 pilot + 4 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 425 m/min 1,395 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.