Airbus A321XLR vs. Bell 412

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Airbus A321XLR versus Bell 412
44.51 m 146 ft 0 in length 17,10 m 56 ft 1 in
11.76 m 38 ft 7 in height 3,48 m 11 ft 5 in
35.8 m 117 ft 5 in wingspan
CFM LEAP-1A and P&W PW1100G engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
33,000 lbs (147 kN) thrust per engine 1,800 hp
66,000 lbs (294 kN) total thrust 3,600 hp
101,000 kg 222,700 lb MTOW 5,400 kg 11,905 lb
4,700 nmi 8,704 km range 659 km 356 nm
963km/h 598mph cruise speed 259 km/h 161 mph
180-220 seats (typical 2-class seating) capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.