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