LWD Junak
Trainer
Photo ©: Karsten Palt
The LWD Junak is a single-engine two-seat trainer aircraft developed by the Polish construction bureau Lotnicze Warsztaty Doswiadczalne (LWD) and produced by the Polish manufacturer WSK-Okecie (WSK Nr 4).
| Crew | 2 | |
| Propulsion | 1 Radial Engine | |
| Engine Model | Shvetsov M-11FR | |
| Engine Power | 118 kW | 158 hp |
| Speed | 206 km/h | 111 kts 128 mph |
| Service Ceiling | 4.100 m | 13.451 ft |
| Range | 450 km | 243 NM 280 mi. |
| Empty Weight | 818 kg | 1.803 lbs |
| max. Takeoff Weight | 1.080 kg | 2.381 lbs |
| Wing Span | 9,92 m | 32 ft 7 in |
| Wing Area | 17,5 m² | 188 ft² |
| Length | 7,75 m | 25 ft 5 in |
| Height | 2,50 m | 8 ft 2 in |
| First Flight | 22.02.1948 | |
| Production Status | out of production | |
| Total Production | 252 | |
| Data for (Version) | LWD Junak 3 | |
| Variants | Junak 1, Junak 2, TS-9 Junak 3, Zuch 1, Zuch 2 | |
| [Photo-ID: 11603] © Karsten Palt 2015-08-22 | |
 | LWD Junak-3 Reg.: SP-BPL c/n: 13-9578 |
| Polish Aviation Museum [Krakow] | |