Mil Mi-17 / Mi-171
Medium Multi-Purpose Helicopter
The Mil Mi-17 is a twin-engined medium utility helicopter developed by the Soviet manufacturer Mil OKB, today MIL Moscow helicopter plant, JSC (Russia).
The Mil Mi-17 is a development of the Mil Mi-8. The Mi-17 is as of today still in production.
| Crew | 3 | |
| Propulsion | 2 Turboshaft Engines | |
| Engine Model | Klimov TW3-117MT / TV3-117MT | |
| Engine Power (each) | 1435 kW | 1924 shp |
| Speed | 250 km/h | 135 kts 155 mph |
| Service Ceiling | 5.000 m | 16.404 ft |
| Range | 494 km | 267 NM 307 mi. |
| Empty Weight | 7.100 kg | 15.653 lbs |
| max. Takeoff Weight | 13.000 kg | 28.660 lbs |
| Rotor Blades (main/tail) | 5/3 | |
| Main Rotor Diameter | 21,10 m | 69 ft 3 in |
| Tail Rotor Diameter | 3,91 m | 12 ft 10 in |
| Rotor Disc Area | 349,7 m² | 3764 ft² |
| Length | 25,30 m | 83 ft 0 in |
| Height | 5,65 m | 18 ft 6 in |
| First Flight | 1975 | |
| Production Status | in production | |
| Developed from | Mil Mi-8 | |
| ICAO Code | MI8 | |
| NATO Code | Hip C | |
| Data for (Version) | Mil Mi-17 | |
| [Photo-ID: 2978] © Hartmut Ehlers 2009-12-01 | |
 | Mil Mi-17-1V Malaysian Government - Fire & Rescue Department Reg.: M994-02 c/n: 95824 |
| LIMA 2009 [Pulau Langkawi - International (WMKL / LGK)] | |