Airbus A319neo vs. Commonwealth CA-25 Winjeel

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Airbus A319neo versus Commonwealth CA-25 Winjeel
33.84 m 111 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
2 x PW 1100G or 2 x CFM LEAP-1A engines 1 x Pratt & Whitney R-985-AN-2 radial engine
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 450 hp
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 450 hp
75,500 kg 166,400 lb MTOW 5,650 lb 2,563 kg
6,850 km 3,702 nm range 1,287 km 695 nm
530 mph 853 km/h cruise speed 150 mph 241 km/h
120-150 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.