Light multipurpose helicopter Ka-266 with two Allison 250-C20R/2 Rolls Royce turboshaft engines with maximum takeoff weight of 3.4 tons is designed for passenger carriage (up to 7 persons) and freight hauling in the transport cabin (up to 1046kg), trade zones patrolling, monitoring and solving other special tasks.
Light multipurpose helicopter Ka-226T with two Arrius 2G1 turboshaft engines and maximum takeoff weight of 4 tons is designed for performing the tasks in hardly accessible areas of highlands, hot climate and above water areas, freight hauling (up to 1630 kg), passenger and staff carriage.
| Takeoff weight | 3400 kg |
|---|---|
| Maximum weight of load in transport cabin | 1046 kg |
| Maximum weight of external load | 1300 kg |
| Maximum speed | 210 km/h |
| Maximum flight altitude | 3500 m |
| Crew | 1 person |
| Maximum length of the load | 1920 mm |
| Maximum width of the load | 1200 mm |
| Maximum height of the load | 1280 mm |
| Maximum altitude of a helipad | 3000 m |
| Takeoff weight | 3600 kg |
|---|---|
| Maximum weight of load in transport cabin | 1046 kg |
| Maximum weight of external load | 1000 kg |
| Maximum weight of the helicopter with external load | 3800 kg |
| Maximum speed | 250 km/h |
| Maximum flight altitude | 7000 m |
| Crew | 2 persons |
| Maximum length of the load | 1920 mm |
| Maximum width of the load | 1200 mm |
| Maximum height of the load | 1280 mm |
| Maximum altitude of a helipad | 6000 m |