Airbus A321XLR vs. Air Tractor AT-802

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Airbus A321XLR versus Air Tractor AT-802
44.51 m 146 ft 0 in length 10.16 m 33 ft 4 in
11.76 m 38 ft 7 in height 3.66 m 12 ft
35.8 m 117 ft 5 in wingspan 18.29 m 60 ft
CFM LEAP-1A and P&W PW1100G engines 1 x Pratt & Whitney Canada PT6A-67F turboprop engine
33,000 lbs (147 kN) thrust per engine 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
66,000 lbs (294 kN) total thrust 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
101,000 kg 222,700 lb MTOW 7,257 kg 16,000 lb
4,700 nmi 8,704 km range 1,125 km 607 nm
963km/h 598mph cruise speed 240 km/h 149 mph
180-220 seats (typical 2-class seating) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.