Tatra T-131
General information
| Manufacturer | Tatra |
| Model | T-131 |
| Modification | T-131 |
| Country | Czechoslovakia |
| Years | 1936 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 7.35 m |
| Length | 6.62 m |
| Height | - |
| Wing area | 13.50 m2 |
| Zero fuel weight | - |
| Empty weight | 375 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 630 kg |
| Flight duration | - |
| Engine | 1 Tatra T-100 (Hirth HM 504 |
| Power | 1 x 100 HP |
| Thrust | - |
| Maximum speed | 190 km/h |
| Cruising speed | 165 km/h |
| Rate of climb | - |
| Practical range | 550 km |
| Service ceiling | 4000 m |
| Hovering ceiling | - |
| Crew | 2 |