McDonnell Douglas A-4 Skyhawk vs. de Havilland Canada DHC-6 Twin Otter

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McDonnell Douglas A-4 Skyhawk versus de Havilland Canada DHC-6 Twin Otter
12.19 m 40 ft 0 in length 15.32 m 50 ft 3 in
4.57 m 15 ft height 5.94 m 19 ft 6 in
8.08 m 26 ft 6 in wingspan 19.81 m 65 ft
1x Pratt & Whitney J52-P-6A Jet engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
8,500 pound-force thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
8,500 pound-force total thrust 1100 to 1500 shaft horsepower
11,113 kg 24,500 lb MTOW 5,670 kg 12,500 lb
3,222 km 1,739 nm range 1,389 km 750 nm
586 kts 364 mph cruise speed 280 km/h 174 mph
Up to 9,155 pounds of weapons on 5 hardpoints 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.