Airbus A321XLR vs. de Havilland Canada DHC-6 Twin Otter

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Airbus A321XLR versus de Havilland Canada DHC-6 Twin Otter
44.51 m 146 ft 0 in length 15.32 m 50 ft 3 in
11.76 m 38 ft 7 in height 5.94 m 19 ft 6 in
35.8 m 117 ft 5 in wingspan 19.81 m 65 ft
CFM LEAP-1A and P&W PW1100G engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
33,000 lbs (147 kN) thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
66,000 lbs (294 kN) total thrust 1100 to 1500 shaft horsepower
101,000 kg 222,700 lb MTOW 5,670 kg 12,500 lb
4,700 nmi 8,704 km range 1,389 km 750 nm
963km/h 598mph cruise speed 280 km/h 174 mph
180-220 seats (typical 2-class seating) capacity 19 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.