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'''[[Mil Moscow Helicopter Plant|Mil]] Mi-26''' ([[Bahasa Rusian|Rusia]] '''Миль Ми-26''', nama yang dilaporkan [[NATO]] "Halo") adalah helikopter pengangkut berat [[Uni Soviet]]/[[Rusia]] yang melayani penduduk dan militer. Helikopter ini merupakan helikopter terbesar dan terkuat yang pernah diproduksi.
==Operator==
===Operator militer===
[[File:Mi-26T.jpg|thumb|]]
[[File:Mil Mi-26TC.jpg|thumb|]]
[[File:Mil-Mi26-0a.jpg|thumb|]]
[[File:MI 26 Helicopter-Giant.jpg|thumb|]]
[[File:Mi-26.jpg|thumb|]]
[[Image:MIL MI-26 Halo.JPG|thumb|right|Mil Mi-26 di Monino Museum (Moskow), 2006]]
[[Image:P1010525x.jpg|thumb|right|]]
;{{BLR}}
;{{COD}}
;{{IND}}
;{{LAO}}
;{{MEX}}
;{{NEP}}
;{{DPRK}}
;{{PER}}
;{{RUS}}
;{{USSR}}
;{{UKR}}
;{{UZB}}
;{{VEN}}
===Operator sipil===
;{{CAN}}
;{{PRC}}
;{{GRE}}
;{{IND}}
;{{ITA}}
;{{LAO}}
;{{PER}}
;{{RUS}}
;{{USSR}}
;{{SUI}}
==Spesifikasi (Mi-26)==
[[Image:Mil Mi-26 HALO.png|300px|right|Mil Mi-26 3-view drawing]]
{{aircraft specifications|
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
<!-- please answer the following questions -->
|plane or copter?=copter
|jet or prop?=prop
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply, like capacity, leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Airtemp]]. -->
|crew=Six – 2 pilots, 1 navigator, 1 flight engineer, 1 loadmaster, 1 radio/electronic systems operator
|capacity=<br/>
**80 troops, 60 litters<ref name="fas">{{cite web |url=http://www.fas.org/man/dod-101/sys/ac/row/mi-26.htm |title=Mi-26 HALO |publisher=fas.org}}</ref>
**20,000 kg cargo (44,000 lbs)<ref name="fas"/>
|length main=40.025 m
|length alt=131 ft 4 in) (rotors turning
|span main=32.00 m
|span alt=104 ft 11.8 in
|li>'''Fuselage width:''' 8.2 m (26 ft 11 in
|height main=8.145 m
|height alt=26 ft 9 in
|area main=789 m<sup>2</sup>
|area alt=8,495 ft²
|empty weight main=28,200 kg
|empty weight alt=62,170 lb
|loaded weight main=49,500 kg
|loaded weight alt=108,900 lb
|max takeoff weight main=56,000 kg
|max takeoff weight alt=123,500 lb
|max payload weight = 20,000kg
|more general=
|engine (prop)=[[Lotarev]] [[Lotarev D-136|D-136]]
|type of prop=[[turboshaft]]s
|number of props=2
|power main=8,380 kW
|power alt=11,240 shp
|max speed main=295 km/h, 183 mph
|max speed alt=160 kt
|ceiling main=4,600 m
|ceiling alt=15,100 ft
|range main=1,952 km, 1,240 miles
|range alt=1,080 nautical miles
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|power/mass main=
|power/mass alt=
}}
== Pranala luar ==
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