SOKO 522
Trainer
The SOKO 522 is a single-engine two seat trainer aircraft produced by the Yugoslav manufacturer SOKO. It was operated by the ex-Yugoslav Air Force until 1978 as a basic trainer.
Propulsion | 1 Radial Engine |
Engine Model | Pratt & Whitney R-1340-AN-1 Wasp |
Engine Power | 447 kW | 600 hp |
max. Cruise Speed | 296 km/h | 160 kts 184 mph |
max. Speed (vne) | 333 km/h | 180 kts 207 mph |
Service Ceiling | 5.070 m | 16.634 ft |
Range | 606 km | 327 NM 376 mi. |
Empty Weight | 2.020 kg | 4.453 lbs |
max. Takeoff Weight | 2.564 kg | 5.653 lbs |
Wing Span | 11,00 m | 36 ft 1 in |
Wing Area | 18,0 m² | 194 ft² |
Length | 8,77 m | 28 ft 9 in |
Height | 3,69 m | 12 ft 1 in |
First Flight | 19.06.1955 |
Production Status | out of production |
Total Production | ca. 110 |
Data for (Version) | SOKO 522 |