| Manufacturer | VEF |
| Model | IDA-10M |
| Modification | IDA-10M |
| Country | Latvia |
| Years | 1939 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.40 m |
| Length | 9.00 m |
| Height | 3.30 m |
| Wing area | 24.00 m2 |
| Zero fuel weight | - |
| Empty weight | 1680 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 2800 kg |
| Flight duration | - |
| Engine | 2 Armstrong Siddeley Cheetah IX |
| Power | 2 x 350 HP |
| Thrust | - |
| Maximum speed | 350 km/h |
| Cruising speed | 280 km/h |
| Rate of climb | 385 m/min |
| Practical range | 560 km |
| Service ceiling | 6800 m |
| Hovering ceiling | - |
| Crew | 2 |
