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ANBO-I was a single-seater low wing monoplane, suitable for pilot training. It was tested on July 14th,
1925. The fuselage was made of welded steel tubing, fabric covered; wings were of wooden construction also fabric covered.
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| ANBO-I |
Technical data:
| Engine |
Anzani
35 HP |
| Empty weight |
190 kg |
| Flight weight |
300 kg |
| Wingspan |
10 m |
| Wing area |
11.4 mē |
| Length |
5.75 m |
| Max.speed |
142 km/h |
| Landing speed |
50 km/h |
| Ceiling |
4.2 km |
Climbing to
1 km altitude
2 km altitude |
6 min.
14 min. |
| Fuel tanks |
45 l |
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