Aviation Project Service| Engine | |
| Conti O 200A | 4 Cylinder |
| T/O power | 100 HP |
| Dimension | |
| Length | 7.2 m |
| Height | 2.6 m |
| Span | 10 m |
| Mass | |
| DOW | 493 KG |
| MTOW | 726 KG |
| Flight performance parameters | |
| Cruising speed | 180 km/h |
| Service ceiling | 12500 ft |
| T/O- and landing distances | |
| T/O roll | 225 m |
| T/O distance | 425 m (with 15m obstacle clearance) |
| Landing roll distance | 140 m |
| Landing distance | 330 m (with 15m obstacle clearance) |