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الطايره يوغنديــــــــــــة
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The Mi-172 helicopter has been continually developed and improved over the past years and is currently under-going commercial certification with the Russian Civil Aviation Authority. In parallel to the Russian certification effort the helicopter is currently being evaluated to show compliance with the latest version of FAA regulation FAR-29 and with the new avionics will meet the requirements for helicopter IFR certification. The derivative Mi-17KF is equipped with Honeywell EDZ-756 Electronic Flight instrument System, Primus II Integrated Radio System, VG14/DG14 Attitude&Heading Reference System, P700 Color Radar and DFZ-706 Flight Director Systems as standard, installed in accordance with the requirements of FAR-29. The cabin is 23 cubic meters in volume (813 cu.ft.), and with large rear clam-shell and sliding side doors the helicopter is ideally suited for various loads including internal vehicle transportation and extra-lenght cargo with open rear ramp.
Specification
PERFORMANCE TV3-117VM engines ..... 2х2200 h.p. Takeoff weight: kg normal ..... 11100 maximum ..... 13000 Cargo mass: kg inside ..... 4000 on external sling ..... 4500 Speed: km/h maximum ..... 250 cruise ..... 230 Hover ceiling: m..... 3980 Service ceiling: m ..... 6000 Range: km .....715 Crew: ..... 3 Number of seats: ..... 36 Number of stretchers:..... 12
للمعلومية فقـــــــــــــــط؟؟؟؟؟؟
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