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R44 | ||
Support and training helicopter | ||
Specification: | ||
Year deployed
Main rotor diametr, m Tail rotor diametr, m Lenght, m Height, m Weight, kg - empty - maximum take-off Engine Power, kW Cruising speed, km/h Combat range, km Rate of climb, m/min Service ceiling, m Static ceiling, m Crew Useful load: |
- 1992 - 10.06 - 2.07 - 8.06 - 3.28 - 635 - 1088 - 1 PE Textron Lycoming н-540 - 1 У 194 - 209 - 643 - - 4270 - 2200 - 2 - 2 passengers |