Airbus A321XLR vs. Commonwealth CA-25 Winjeel

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 1 x Pratt & Whitney R-985-AN-2 radial engine
33,000 lbs (147 kN) thrust per engine Approximately 450 hp
66,000 lbs (294 kN) total thrust Approximately 450 hp
101,000 kg 222,700 lb MTOW 5,650 lb 2,563 kg
4,700 nmi 8,704 km range 1,287 km 695 nm
963km/h 598mph cruise speed 150 mph 241 km/h
180-220 seats (typical 2-class seating) 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.