Airbus A220-100 vs. Commonwealth CA-25 Winjeel

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Airbus A220-100 versus Commonwealth CA-25 Winjeel
35.0 m 114 ft 10 in length 7.77 m 25 ft 6 in
11.5 m 37 ft 9 in height 2.84 m 9 ft 4 in
35.1 m 115 ft 2 in wingspan 10.82 m 35 ft 6 in
2 Turbofans (wing mounted) engines 1 x Pratt & Whitney R-985-AN-2 radial engine
21,000–23,000 lb thrust per engine Approximately 450 hp
42,000–46,000 lb total thrust Approximately 450 hp
63,100 kg 139,100 lb MTOW 5,650 lb 2,563 kg
6,390 km 3,451 nm range 1,287 km 695 nm
871 km/h 541 mph cruise speed 150 mph 241 km/h
Typical seating 2-class 100-120 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.