Airbus A310-300 vs. Bell 206

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Airbus A310-300 versus Bell 206
46.66 m 153 ft 1 in length 12.11 m 39 ft 9 in
15.8 m 51 ft 10 in height 2.88 m 9 ft 5 in
43.9 m 144 ft wingspan
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 × Allison 250-C20B
52,000 lb thrust per engine 420 shp (313 kW)
104,000 lb total thrust 420 shp (313 kW)
148,768 kg 328,000 lb MTOW 1,451 kg 3,199 lb
8,050 km 4,348 nm range 374 km 202 nm
482 knots 279 mph cruise speed 222 km/h 138 mph
190-230 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.