Airbus A310-300 vs. Commonwealth CA-25 Winjeel

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Airbus A310-300 versus Commonwealth CA-25 Winjeel
46.66 m 153 ft 1 in length 7.77 m 25 ft 6 in
15.8 m 51 ft 10 in height 2.84 m 9 ft 4 in
43.9 m 144 ft wingspan 10.82 m 35 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Pratt & Whitney R-985-AN-2 radial engine
52,000 lb thrust per engine Approximately 450 hp
104,000 lb total thrust Approximately 450 hp
148,768 kg 328,000 lb MTOW 5,650 lb 2,563 kg
8,050 km 4,348 nm range 1,287 km 695 nm
482 knots 279 mph cruise speed 150 mph 241 km/h
190-230 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.