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 210
- from water 350

Landing roll (ISA, sea level), m
- on ground 190
- on water 270

Minimum operation depth of the water reservoir, m 0.9
Wave height, m 0.45
Crew, person 1
Passengers, persons 3