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).
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