Airbus A220-100 vs. N. American T-28 Trojan

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Airbus A220-100 versus N. American T-28 Trojan
35.0 m 114 ft 10 in length 10.06 m 33 ft 0 in
11.5 m 37 ft 9 in height 3.86 m 12 ft 8 in
35.1 m 115 ft 2 in wingspan 12.22 m 40 ft 1 in
2 Turbofans (wing mounted) engines 1 x Wright R-1820-86 Cyclone radial engine
21,000–23,000 lb thrust per engine Approximately 1,425 hp
42,000–46,000 lb total thrust Approximately 1,425 hp
63,100 kg 139,100 lb MTOW 8,500 lb 3,856 kg
6,390 km 3,451 nm range 1,705 km 921 nm
871 km/h 541 mph cruise speed 210 mph 338 km/h
Typical seating 2-class 100-120 capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.