Lockheed Martin F-35 Lightning II vs. de Havilland Canada DHC-6 Twin Otter

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Lockheed Martin F-35 Lightning II versus de Havilland Canada DHC-6 Twin Otter
15.67 m 51 ft 4 in length 15.32 m 50 ft 3 in
4.33 m 14 ft 2 in height 5.94 m 19 ft 6 in
10.7 m 35 ft 1 in wingspan 19.81 m 65 ft
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
40,000 lb thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
40,000 lb total thrust 1100 to 1500 shaft horsepower
31,800 kg 70,000 lb MTOW 5,670 kg 12,500 lb
1,380 mi 1,200 nm range 1,389 km 750 nm
520 kt 302 mph cruise speed 280 km/h 174 mph
18,000 pounds of total ordinance capacity 19 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.