Airbus A220-100 vs. Lockheed Martin F-35 Lightning II

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Airbus A220-100 versus Lockheed Martin F-35 Lightning II
35.0 m 114 ft 10 in length 15.67 m 51 ft 4 in
11.5 m 37 ft 9 in height 4.33 m 14 ft 2 in
35.1 m 115 ft 2 in wingspan 10.7 m 35 ft 1 in
2 Turbofans (wing mounted) engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
21,000–23,000 lb thrust per engine 40,000 lb
42,000–46,000 lb total thrust 40,000 lb
63,100 kg 139,100 lb MTOW 31,800 kg 70,000 lb
6,390 km 3,451 nm range 1,380 mi 1,200 nm
871 km/h 541 mph cruise speed 520 kt 302 mph
Typical seating 2-class 100-120 capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.