Airbus A220-300 vs. N. American T-28 Trojan

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Airbus A220-300 versus N. American T-28 Trojan
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 8,500 lb 3,856 kg
6,297 km 3,402 nm range 1,705 km 921 nm
Mach 0.82 101,3 km/h cruise speed 210 mph 338 km/h
Typical seating 2-class 120-150 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.