Lockheed P-2 Neptune vs. Cessna 208 Caravan
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Lockheed P-2 Neptune |
versus |
Cessna 208 Caravan |
30.17 m |
99 ft 0 in |
length |
12.67 m |
41 ft 7 in |
10.15 m |
33 ft 4 in |
height |
4.49 m |
14 ft 9 in |
33.53 m |
110 ft |
wingspan |
15.88 m |
52 ft 1 in |
2 x Wright R-3350 radial engines |
engines |
1 x Pratt & Whitney Canada PT6A-114A turboprop engine |
Approximately 3,700 hp |
thrust per engine |
675 shaft horsepower (503 kW) |
Approximately 7,400 hp |
total thrust |
675 shaft horsepower (503 kW) |
27,216 kg |
60,000 lb |
MTOW |
4,740 kg |
10,450 lb |
7,885 km |
4,259 nm |
range |
1,777 km |
960 nm |
300 mph |
483 km/h |
cruise speed |
340 km/h |
211 mph |
based on configuration |
capacity |
Up to 14 passengers or 3,034 kg |
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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.