lockheed C-130 hercules vs. de Havilland Canada DHC-6 Twin Otter
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| lockheed C-130 hercules |
versus |
de Havilland Canada DHC-6 Twin Otter |
| 29.79 m |
97 ft 9 in |
length |
15.32 m |
50 ft 3 in |
| 11.66 m |
38 ft 3 in |
height |
5.94 m |
19 ft 6 in |
| 40.41 m |
132 ft 7 in |
wingspan |
19.81 m |
65 ft |
| 4 x Allison T56-A-15 turboprop engines |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
| Approximately 4,590 hp per engine |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
| Approximately 18,360 hp total |
total thrust |
1100 to 1500 shaft horsepower |
| 70,307 kg |
155,000 lb |
MTOW |
5,670 kg |
12,500 lb |
| 3,760 km |
2,031 nm |
range |
1,389 km |
750 nm |
| 540 km/h |
335 mph |
cruise speed |
280 km/h |
174 mph |
| based on configuration |
capacity |
19 passengers |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.
