Airbus A321LR vs. Air Tractor AT-802

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Airbus A321LR 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 International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Pratt & Whitney Canada PT6A-67F turboprop engine
Over 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)
97,000 kg 213,800 lb MTOW 7,257 kg 16,000 lb
7,400 km 4,000 nm range 1,125 km 607 nm
832 km/h 517 mph cruise speed 240 km/h 149 mph
180-220 passengers 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.