Engine for M-601 aircraft
Vendor code: 130313 27 April 6 0
Engine M-601 for aircraft L-410
We will send information on developments and copies of forms after receiving an official application from the customer.
Engine M-601 is a turboprop aircraft engine developed for the Let L-410 aircraft.
Main technical characteristics:
| Parameter | Meaning |
|---|---|
| Type | Turboprop, with free turbine |
| Application | Let L-410 aircraft and their modifications |
| Construction | Modular (gas generator, drive part) |
| Power (max. mode) | up to 630 kW (850 hp) |
| Diameter | ~1.2 m (depending on modification) |
| Weight | about 250–300 kg |
| Fuel | Aviation kerosene |
| propeller | Five-blade, variable pitch |
| Features | Reverse flow of air and gases, high reliability, modular design |
Modifications:
- M601A - basic option for early L-410.
- M601B — for L-410UVP.
- M601D — for L-410UVP, with increased resource.
- M601D-1, D-2, D-11 — specialized versions for agricultural aviation and landing operations.
M-601 It is characterized by high reliability, ease of maintenance and a long service life between repairs. Widely used on regional and special aircraft, as well as in civil aviation educational institutions.
- State: Rebuilt
- Documents: Sold with documents
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