Airbus A320-200 vs. Commonwealth CA-25 Winjeel

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Airbus A320-200 versus Commonwealth CA-25 Winjeel
38.7 m 127 ft 0 in length 7.77 m 25 ft 6 in
17.4 m 57 ft 1 in height 2.84 m 9 ft 4 in
35.8 m 117 ft 5 in wingspan 10.82 m 35 ft 6 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 x Pratt & Whitney R-985-AN-2 radial engine
Between 21,000 - 33,000 lbf thrust per engine Approximately 450 hp
Between 42,000 - 66,000 lbf total thrust Approximately 450 hp
77,000 kg 169,800 lb MTOW 5,650 lb 2,563 kg
5,700 km 3,078 nm range 1,287 km 695 nm
530 mph 853 km/h cruise speed 150 mph 241 km/h
Typically between 140-180 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.