Airbus A320neo vs. Commonwealth CA-25 Winjeel

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Airbus A320neo versus Commonwealth CA-25 Winjeel
37.57 m 123 ft 3 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
2 x PW 1100G or 2 x CFM LEAP-1A engines 1 x Pratt & Whitney R-985-AN-2 radial engine
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 450 hp
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 450 hp
79,000 kg 174,200 lb MTOW 5,650 lb 2,563 kg
6,300 km 3,403 nm range 1,287 km 695 nm
M0.82 101,3 km/h cruise speed 150 mph 241 km/h
150-180 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.