Airbus A319neo vs. Lockheed Martin F-35 Lightning II

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Airbus A319neo versus Lockheed Martin F-35 Lightning II
33.84 m 111 ft 0 in length 15.67 m 51 ft 4 in
11.76 m 38 ft 7 in height 4.33 m 14 ft 2 in
35.8 m 117 ft 5 in wingspan 10.7 m 35 ft 1 in
2 x PW 1100G or 2 x CFM LEAP-1A engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 40,000 lb
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 40,000 lb
75,500 kg 166,400 lb MTOW 31,800 kg 70,000 lb
6,850 km 3,702 nm range 1,380 mi 1,200 nm
530 mph 853 km/h cruise speed 520 kt 302 mph
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.