Airbus A300-600F vs. Bell 206

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Airbus A300-600F versus Bell 206
54.08 m 177 ft 5 in length 12.11 m 39 ft 9 in
17.05 m 55 ft 11 in height 2.88 m 9 ft 5 in
44.84 m 147 ft 1 in wingspan
2 x General Electric CF6-80C2A5 turbofan engines engines 1 × Allison 250-C20B
Approximately 59,000 lbf per engine thrust per engine 420 shp (313 kW)
Approximately 118,000 lbf total total thrust 420 shp (313 kW)
170,000 kg 374,786 lb MTOW 1,451 kg 3,199 lb
4,830 km 2,608 nm range 374 km 202 nm
860 km/h 534 mph cruise speed 222 km/h 138 mph
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.