The amphibious features of the Be-103 aircraft provide for its wide use in various regions abundant in rivers, lakes, water reservoirs difficult of access for other types of transport.

The aircraft is fitted with flight/navigation and communication equipment which enables its operation in adverse weather conditions, in daytime and nighttime. Be-103 can accommodate five passengers, the aircraft cabin layout provides for passengers comfort during flight.

At customer's option, the aircraft can be equipped with autopilot, satellite navigation system, weather radar.

Any of aircraft variants can also be fitted with work station for copilot (instructor).

The Be-103 amphibious aircraft has been designed in compliance with airworthiness requirements of FAR-23 (USA) and AR-23 (Russia).

OVERALL DIMENSIONS
Wing span, m 12.72
Aircraft lenght, m 10.65
Aircraft height, m 3.757
Wing area, m2 25.1
Wheelbase, m 4.064
Track 2.273
Cabin:
- Length, m 3.38
- Height, m 1.23
- Maximum width, m 1.25
WEIGHTS
Operational empty weight, kg 1,834
Operational weight, kg 1,902
Maximum take-off weight (ground, water), kg 2270
Maximum landing weight (ground, water), kg 2270
Maximum fuel capacity, kg 245
Maximum payload, kg 368
PERFORMANCE
Maximum cruise speed (ISA, 3,000 m), km/h 240
Ecocnomic cruise speed (ISA, 3,000 m), km/h 190-210
Operational altitude, m 3,000
Service ceiling, m 5020
Maximum range (ISA, 3,000 m, 0.5 hour fuel reserve), km 1070
Take-off run (ISA, sea level) (ground/water), m 350/560
Landing roll (ISA, sea level) (ground/water), m 400/360
Seaworthiness:
- Sea state 2
- Wave height, m 0.5
Minimum depth of water for operations, m 1.25
Engine type TCM-IO-360ES4
Number and power, h.p. 2 x 210

Crew, prs. 2
Numbur of passenger seats 5