In numbers Through the lens Video
The GTD-350 is a small, single-stage turboshaft engine with a free turbine and a takeoff power of 400 hp. It features an axial-centrifugal compressor consisting of (seven axial stages and one centrifugal stage), a single-stage compressor turbine, a tubular combustion chamber, a two-stage free turbine, and an intermediate gearbox.

GTD-350 (left view). Dimensional drawing.
Mass production of the engine began in 1963 and continued until the late 1990s.
From 1964 onward, the GTD-350 turboshaft engine, together with the VR-2 gearbox, was mass-produced at the Polish WSK PZL Świdnik plant. In total, more than 11,000 units were manufactured.

GTD-350 (front view and rear view). Dimensional drawing.
Technical specifications
| DESIGNER | JSC Klimov |
| COUNTRY | Russia |
| TYPE |
Turboshaft engine
|
| Installed On (aerial means) |
Mi-2
|
| Fuel | Aviation kerosene, JP-4 |
| Oil | - |
| Propeller shaft power, take-off power rating | 400 h.p. |
| Specific fuel consumption, take-off power rating | 0,365 kg/h.p.*h |
| Propeller shaft power, cruise power | - |
| Specific fuel consumption, cruise power | - |
| Pressure ratio, take-take-off power rating | 6,0 |
| Temperature of the gas at the turbine intake, take-off power rating | 1.243 K |
| Air flow rate, take-off power rating | 2,2 kg/sec |
| OVERALL DIMENSIONS | |
| Diameter | - |
| Height | 680 mm |
| Width | 522 mm |
| Length | 1350 mm |
| WEIGHT | |
| Engine weight | 135 kg |
| Specified service life | 4.000 h |