Comparison of Kazan Mi-17 and Mil Mi-8 “Hip” [S]ave
| Attribute |  Kazan Mi-17 × |  Mil Mi-8 “Hip” × |
|---|---|---|
| General | ||
| Manufacturer | Kazan Helicopters | MIL Helicopters |
| Model | Kazan Mi-17 | Mil Mi-8 “Hip” |
| Country | Russia | Russia |
| Manufactured from (year) | 2005 | 1961 |
| Type | Large Helicopters | Military Helicopters |
| Icao | MI17 | - |
| Performance | ||
| Engine | 2 × Klimov TV3-117VM turboshafts - | 2 × Klimov TV3-117Mt turboshafts - |
| Power, hp (hp) | 1,950 | 1,950 |
| Max cruise speed (km/h) | 230 | 224 |
| Travel range (km) | 465 | 959 |
| Fuel economy (km/l) | 0.22 | 0.298 |
| Service ceiling (m) | 6,000 | 4,500 |
| Rate of climb (m/sec) | 8 | 8.99 |
| Weights | ||
| Max take off weight (kg) | 13,000 | 12,000 |
| Max payload (kg) | 4,000 | 3,000 |
| Fuel tank capacity (l) | 3,698 | 3,702 |
| Dimensions | ||
| Seats | 36 | 28 |
| Seats - business class | 26 | - |
| Seats - first class | 11 | - |
| Cabin height (m) | 1.8 | 1.26 |
| Cabin width (m) | 2.34 | 1.2 |
| Cabin length (m) | 5.34 | - |
| Exterior length (m) | 18.47 | 18.17 |
| Tail height (m) | 5.65 | - |
| Fuselage diameter (m) | 2.5 | - |
| Wing span (m) | 21.3 | 21.29 |
| Wing tips | No Winglets | No Winglets |
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