| Technical data | |
|---|---|
| Type | Mi-17-1VA |
| Function | utility |
| Year | 1980 |
| Crew | ? |
| Engines | 2*2250(1950?)hp Isotov TV-3-117VM |
| Rotor Span | 21.2m |
| Length | 25.3m |
| Height | 4.70m |
| Disc Area | 365m2 |
| Empty Weight | 7100kg |
| Maximum Weight | 13000kg |
| Speed | 262(250?)km/h |
| Ceiling | 6000(5000?)m |
| Range | 465(495?)km |
| Load | 4000kg or 24 seats |
Mi-17, M.L.Mil 'Hip-H'
|
Improved Mi-8, with more powerful engines for 'hot and high' conditions. The designation Mi-17 is for export; the USSR armed forces called it Mi-8MT. The Mi-17 can be recognized because it has the tail rotor at the starboard side, instead of the port side.
| Predecessors | Modifications | Developments |
|---|---|---|
 Mi-8 |
? |
More Links...
- Mi-17, Mi-171, Mi-172
- Mi-17
- Mi-17 at Mil Moscow Helicopters Plant
- The International Workhorse - the Mi-17
- Kazan Helicopters Plant is a manufacturer of the Mi-17 and its variants
- RUSSIA INTENDS TO EXPAND EXPORT OF Mi-17-1V HELICOPTERS
- MAKS-97 overview
- Mi-8/9/...
- Mi-17, Mil 'Hip'
- Mi-17MD HELICOPTER: VERSATILE CAPABILITIES;
