| KEY DATA |
| Crew |
Three (Pilot, Navigator, Flight
Mechanic) |
| Equipped troops |
24 |
| Passengers |
36 |
| Stretchers |
12 |
| DESIGN |
| Designer |
Mil Design Bureau |
| Manufacturer |
Ulan-Ude Aviation Plant (Mi-17, Mi-171)
Kazan Helicopter Plant JSC (Mi-17-V5, Mi-17V7) |
| DIMENSIONS |
| Fuselage length (without rotors) |
18.22m |
| Height (without rotors) |
5.70m |
| Fuselage width (without rotors) |
2.50m |
| Main rotor blades |
5 |
| Tail rotor blades |
3 |
| WEIGHTS |
| Empty |
Mi-17/171: 7,055kg
Mi-17V5: 7,340kg
Mi-17V7: N/A |
| Normal take-off |
Mi-17/171: 13,000kg
Mi-17V5: 13,000kg
Mi-17V7: 11,100kg |
| Max take-off |
Mi-17/171: 13,000kg
Mi-17V5: 13,000kg
Mi-17V7: 13,500kg |
| Max internal payload |
4,000kg |
| Max external payload on sling |
3,000kg (Mi-17/171), or 3,000~5,000kg (Mi-17V5/V7) |
| PROPULSION |
| Powerplant |
Mi-17/171: 2X TV3-117MT turboshaft, 1,950hp each
Mi-17V5: 2X TV3-117VM(A), 2,200hp each
Mi-17V7: 2X BK2500 turboshaft, 2,400hp each |
| Auxiliary |
Russian APU; or Czech SAFIR 5K/G APU (Mi-17V-7) |
| PERFORMANCE |
| Max speed |
215km/h (normal poayload); 250km/h (max payload) |
| Cruising speed |
215km/h (normal poayload); 230km/h (max payload) |
| Service ceiling |
6,000m (normal poayload); 4,800m (max payload), or 6,200m on normaly payload for Mi-17V7 |
| Hover ceiling (in ground effect) |
Mi-17/171/17-V5: 3,980m (normal payload); 1,700m (max payload)
Mi-17V7: 5,150m (normal payload); 3,980m (max payload) |
| Max range |
600km (main tank only)
800km (with one internal tank)
1,160km (with two internal tanks)
1,720km (with four internal tanks) |
| ARMAMENTS |
| Fixed weapon |
None |
| External hardpoints |
Six |
| Air-to-ground weapons |
12.7mm machine gun pod;
57/90mm rocket launcher |
| Air-to-air missile |
TY-90 |
