Sikorsky S-39
Amphibious Utility Aircraft
The Sikorsky S-39 is a single-engine five-seat amphibious utility aircraft produced by the US-American manufacturer Sikorsky Aviation Corporation, today Sikorsky Aircraft Corporation.
Propulsion | 1 Radial Engine |
Engine Model | Pratt & Whitney R-985 Wasp Junior A |
Engine Power | 224 kW | 300 hp |
max. Cruise Speed | 161 km/h | 87 kts 100 mph |
max. Speed (vne) | 193 km/h | 104 kts 120 mph |
Service Ceiling | 5.486 m | 18.000 ft |
Range | 741 km | 400 NM 460 mi. |
Empty Weight | 1.215 kg | 2.678 lbs |
max. Takeoff Weight | 1.814 kg | 4.000 lbs |
Wing Span | 15,85 m | 52 ft 0 in |
Wing Area | 32,5 m² | 350 ft² |
Length | 9,73 m | 31 ft 11 in |
Height | 3,66 m | 12 ft 0 in |
First Flight | 24.12.1929 |
Production Status | out of production |
Production Range | 1930-1932 |
Total Production | 21 |
Developed from | Sikorsky S-38 |
ICAO Code | S39 |
Data for (Version) | Sikorsky S-39B |