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The Be-101 light amphibian is intended for commercial and non-commercial operations. The aircraft will be certified in compliance with Russian airworthiness regulations AP-23, Europe CS-23 and U.S. FAR-23.
The amphibian is equipped with piston engine IO-550-N (Teledyne Continental Motors, USA), 310 h.p. takeoff power, with pushing propeller MTV-9 (MT-Propeller, Germany).
Aircraft Performance
| OVERALL DIMENSIONS |
|
| Wing span, m |
11.94 |
| Aircraft lenght, m |
9.22 |
| Aircraft height, m |
3.17 |
| Cabin: |
|
| - Length, m |
2.76 |
| - Height, m |
1.3 |
| - Maximum width , m |
1.28 |
| Cargo compartment floor area, m2 |
0.6 |
| WEIGHT |
|
| Maximum takeoff weight (ground, water), kg |
1,570 |
| Maximum payload , kg |
255 |
| Maximum fuel reserve, kg |
140 |
| PERFORMANCE |
|
| Operational altitude, m |
3,000 |
| Maximum cruise speed (ISA, 3,000 m), km/h |
275 |
| Ecocnomic cruise speed (ISA, 3,000 m), km/h |
200 |
| Service ceiling, m |
6,400 |
| Maximum range (ISA, 3000 m, 30 min fuel reserve), km |
1,000 |
Takeoff run on water, m
- from ground
- from water
|
210
350 |
Landing roll (ISA, sea level), m
- on ground
- on water |
190
270 |
| Minimum operation depth of the water reservoir, m
|
0.9 |
| Wave height, m |
0.45 |
| Crew, person |
1 |
| Passengers, persons |
3 |
General View of Aircraft
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