Airbus A220-100 vs. North American T-2 Buckeye

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Airbus A220-100 versus North American T-2 Buckeye
35.0 m 114 ft 10 in length 11.67 m 38 ft 4 in
11.5 m 37 ft 9 in height 4.51 m 14 ft 10 in
35.1 m 115 ft 2 in wingspan 11.62 m 38 ft 1 in
2 Turbofans (wing mounted) engines Two General Electric J85-GE-4 turbojet engines
21,000–23,000 lb thrust per engine 2,950 lbf
42,000–46,000 lb total thrust 5,900 lbf
63,100 kg 139,100 lb MTOW 13,179 lb 5,977 kg
6,390 km 3,451 nm range 1,685 km 909 nm
871 km/h 541 mph cruise speed 453 kts 281 mph
Typical seating 2-class 100-120 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.