Airbus A321LR vs. Commonwealth CA-25 Winjeel

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Airbus A321LR versus Commonwealth CA-25 Winjeel
44.51 m 146 ft 0 in length 7.77 m 25 ft 6 in
11.76 m 38 ft 7 in height 2.84 m 9 ft 4 in
35.8 m 117 ft 5 in wingspan 10.82 m 35 ft 6 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Pratt & Whitney R-985-AN-2 radial engine
Over 33,000 lbs (147 kN) thrust per engine Approximately 450 hp
66,000 lbs (294 kN) total thrust Approximately 450 hp
97,000 kg 213,800 lb MTOW 5,650 lb 2,563 kg
7,400 km 4,000 nm range 1,287 km 695 nm
832 km/h 517 mph cruise speed 150 mph 241 km/h
180-220 passengers capacity Instructor pilot and one student
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.