Airbus A321XLR vs. de Havilland Canada DHC-3 Otter

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Airbus A321XLR versus de Havilland Canada DHC-3 Otter
44.51 m 146 ft 0 in length 10.52 m 34 ft 6 in
11.76 m 38 ft 7 in height 3.84 m 12 ft 7 in
35.8 m 117 ft 5 in wingspan 17.68 m 58 ft
CFM LEAP-1A and P&W PW1100G engines 1 x Pratt & Whitney R-1340 radial engine
33,000 lbs (147 kN) thrust per engine 400 to 600 horsepower (298 to 447 kW)
66,000 lbs (294 kN) total thrust 400 to 600 horsepower (298 to 447 kW)
101,000 kg 222,700 lb MTOW 5,670 kg 12,500 lb
4,700 nmi 8,704 km range 1,296 km 700 nm
963km/h 598mph cruise speed 215 km/h 134 mph
180-220 seats (typical 2-class seating) capacity 10-11 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.