In numbers Through the lens Video
Lightweight, multi-purpose, transport-passenger amphibious aircraft with two turboprop engines of the PT6A-67R type (Pratt Whitney) with a power of 2.848 hp (2x1.424 hp) takeoff power. The power plant is located on both vertical stabilizers with pulling propellers. The aircraft is made according to the scheme of a cantilever monoplane with a high-wing trapezoidal wing. The plumage is two-vertical stabilizer (two keel) with tail unit of type «Τ» and horizontal tail between the vertical stabilizer (keels) with consoles.
Technical specifications
| DESIGNER | OKB Beriev |
| COUNTRY | Russia |
| TYPE |
Amphibian aircraft
|
| CREW | 2 |
| POWER-PLANT | Two turboprop engines TVD-1500 or two Pratt Whitney PT6A-67R |
| Power h.p. | 2x1.424 |
| DIMENSIONS | |
| Length, m | 17,00 |
| Height, m | 5,2 |
| Wing span, m | 21,2 |
| Wing area, m2 | - |
| Cabin dimensions: | |
| - length, m | 10,2 |
| - width, m | 2,15 |
| - height, m | 1,84 |
| Payload, kg | |
| - passenger, seats | 27 |
| LANDING GEAR | |
| Wheel base, m | 8,65 |
| Wheel track, m | 4,5 |
| WEIGHT | |
| Maximum take-off, kg | 11.000 |
| Normal take-off, kg | - |
| Empty aircraft, kg | - |
| Internal fuel, kg | - |
| Payload, kg | 2.350 |
| PERFORMANCE | |
| Maximum speed (H=3.000 m), km/h | 420 |
| Cruising speed, km/h | 370 |
| Range, ( pay load 2.100 kg, H=3.000, + fuel reserve 30 min), km | 1.000 |
| Operational flight ceiling, m | 3.000 |
| Service ceiling, m | 6.000 |
| Take-off run (ISA, sea level), m | |
| - ground | 850 |
| - water | 515 |