Lockheed Martin F-35 Lightning II vs. de Havilland Canada DHC-3 Otter

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Lockheed Martin F-35 Lightning II versus de Havilland Canada DHC-3 Otter
15.67 m 51 ft 4 in length 10.52 m 34 ft 6 in
4.33 m 14 ft 2 in height 3.84 m 12 ft 7 in
10.7 m 35 ft 1 in wingspan 17.68 m 58 ft
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 1 x Pratt & Whitney R-1340 radial engine
40,000 lb thrust per engine 400 to 600 horsepower (298 to 447 kW)
40,000 lb total thrust 400 to 600 horsepower (298 to 447 kW)
31,800 kg 70,000 lb MTOW 5,670 kg 12,500 lb
1,380 mi 1,200 nm range 1,296 km 700 nm
520 kt 302 mph cruise speed 215 km/h 134 mph
18,000 pounds of total ordinance capacity 10-11 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.