Airbus A220-300 vs. North American T-6 Texan

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Airbus A220-300 versus North American T-6 Texan
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 5,617 lb 2,548 kg
6,297 km 3,402 nm range 1,175 km 634 nm
Mach 0.82 101,3 km/h cruise speed 145 mph 233 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.