Airbus A321neo vs. Commonwealth CA-25 Winjeel

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Airbus A321neo 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
35,000 lb thrust per engine Approximately 450 hp
70,000 lb 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
828 km/h 514 mph cruise speed 150 mph 241 km/h
180 to 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.