الطايره يوغنديــــــــــــة

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

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