Airbus A321XLR vs. Bell 206

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Airbus A321XLR versus Bell 206
44.51 m 146 ft 0 in length 12.11 m 39 ft 9 in
11.76 m 38 ft 7 in height 2.88 m 9 ft 5 in
35.8 m 117 ft 5 in wingspan
CFM LEAP-1A and P&W PW1100G engines 1 × Allison 250-C20B
33,000 lbs (147 kN) thrust per engine 420 shp (313 kW)
66,000 lbs (294 kN) total thrust 420 shp (313 kW)
101,000 kg 222,700 lb MTOW 1,451 kg 3,199 lb
4,700 nmi 8,704 km range 374 km 202 nm
963km/h 598mph cruise speed 222 km/h 138 mph
180-220 seats (typical 2-class seating) 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.