Airbus A350-900ULR vs. Bell 206

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Airbus A350-900ULR versus Bell 206
66.80 m 219 ft 2 in length 12.11 m 39 ft 9 in
17.05 m 55 ft 11 in height 2.88 m 9 ft 5 in
64.75 m 212 ft 5 in wingspan
2 Rolls-Royce Trent XWB engines 1 × Allison 250-C20B
84,000 lbs thrust per engine 420 shp (313 kW)
168,000 lbs total thrust 420 shp (313 kW)
280,000 kg 617,300 lb MTOW 1,451 kg 3,199 lb
17,964 km 9,700 nm range 374 km 202 nm
552 mph 888 km/h cruise speed 222 km/h 138 mph
300-350 passengers in three classes 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.