Airbus A220-100 vs. North American T-6 Texan

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Airbus A220-100 versus North American T-6 Texan
35.0 m 114 ft 10 in length 9.0 m 29 ft 6 in
11.5 m 37 ft 9 in height 3.56 m 11 ft 8 in
35.1 m 115 ft 2 in wingspan 12.8 m 42 ft
2 Turbofans (wing mounted) engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
21,000–23,000 lb thrust per engine Approximately 600 hp
42,000–46,000 lb total thrust Approximately 600 hp
63,100 kg 139,100 lb MTOW 5,617 lb 2,548 kg
6,390 km 3,451 nm range 1,175 km 634 nm
871 km/h 541 mph cruise speed 145 mph 233 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.