| Technical data |
|---|
| Type |
MAI-89U, Aviatika-890U |
| Function |
Trainer, sport |
| Year |
1992 |
| Crew |
2 |
| Engines |
1*64hp 'Rotax-582' |
| Length |
5.5m |
| Height |
2.25m |
| Wingspan |
8.11m |
| Wing area |
14.29m2 |
| Empty weight |
235kg |
| Loaded weight |
450kg |
| Wing Load (kg/m2) |
31.5 |
| Power load (kg/hp) |
7.0 |
| Maximum Speed |
125km/h |
| Fuel consumption |
25kg/h |
| Cruise Speed |
90 to 100km/h |
| Fuel consumption |
12kg/h |
| Stall Speed |
57km/h |
| Landing Speed |
68km/h |
| Landing Roll |
110m |
| Takeoff Speed |
72km/h |
| Takeoff Roll |
80m |
| Turn radius |
50m |
| Service G-limits |
+4-2 |
| Range |
270km |
| Flight Endurance |
3.5h |
| Ceiling |
4000m |
| Climb |
| at 0m |
3.0m/sec |
| Payload |
|---|
| Fuel |
40kg |
| Cargo |
120kg |
Shortly
after single-seater MAI-89 proved to be a success, two-seater
twin-controls primary trainer was put in mass production (June
1992).
It differs by cabin arrangement and have different instrument panel.
;)
