Airbus A220-300 vs. Lockheed Martin F-35 Lightning II

versus
... or view the full comparison list here.
Airbus A220-300 versus Lockheed Martin F-35 Lightning II
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 31,800 kg 70,000 lb
6,297 km 3,402 nm range 1,380 mi 1,200 nm
Mach 0.82 101,3 km/h cruise speed 520 kt 302 mph
Typical seating 2-class 120-150 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.