| 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 |
50k in-flight photo from Aviatika-890 page at Aviatika-890 page at Antoine de Saint-Exupery aeroclub.
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.
| References |
Links |
- 'Face of Conversion - MAI-89' by Kazimir Zhidovetski, 'Krylia Rodiny', Dec 1991, pp0...3
|
- Aviatika-890 page at Antoine de Saint-Exupery aeroclub
- Aviatika-890
- MAKS-97
- Aviatika MAI 89/89U
- ANNOUNCEMENT TO ALL PRESENT AND PROSPECTIVE AVIATIKA OWNERS
- Aviatika
- Aviatika MAI 890U ZU-BGL
|
;)
