Small utility helicopter. Most of the fuselage is rectangular, removable box.
| Technical data | ||
|---|---|---|---|
| Type | Ka-26 | ||
| Function | utility | ||
| Year | 1970 | ||
| Crew | 1-2 | ||
| Engines | 2*325hp Vedeneyev M-14V-26 | ||
| Rotor diameter | 42 feet 8 inches | ||
| Speed | 170km/h | ||
| Ceiling | 3000m | ||
| Range | 1200km | ||
| Empty Weight | 4300lb | ||
| Load | 900kg | ||
| Gross Weight | 7165lb | ||
| Modified August 19, 1997
by Alexandre Savine; |
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