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three Mi26 Helicopters SOLD

all based in Europe. All three helicopters are civil registered and therefore have no limitations for such use.

General characteristics

  •  Crew: Five– 2 pilots, 1 navigator, 1 flight engineer, 1 flight technician

  •  Capacity:

  •  90 troops or 60 stretchers

  •  20,000 kg cargo (44,090 lb)

  •  Length: 40.025 m (131 ft 3¾ in) (rotors turning)

  •  Rotor diameter: 32.00 m (105 ft 0 in)

  •  Height: 8.145 m (26 ft 8¾ in)

  •  Disc area: 804.25 m2 (8,656.8 ft²)

  •  Empty weight: 28,200 kg (62,170 lb)

  •  Loaded weight: 49,600 kg (109,350 lb)

  •  Max. takeoff weight: 56,000 kg (123,450 lb)

  •  Powerplant: 2 × Lotarev D-136 turboshafts, 8,500 kW (11,399 shp) each

Performance

  •  Maximum speed: 295 km/h (159 kt, 183 mph)

  •  Cruise speed: 255 km/h (137 kt, 158 mph)

  •  Range: 1,920 km (1,036 nmi, 1,190 mi) (with auxiliary tanks)

  •  Service ceiling: 4,600 m (15,100 ft)

Price: $15.5 million dollars usa

 

 

MI-26  The general Type & biggest helicopter in the world - the Heavy military-transport helicopter Firm - ОКБ him. M.L.mile Year of the beginning of designing - 1972.  Crew - 5.    No of passengers - 80. The size of the helicopter is Length, 40.02 metres;  Height, 8.15 metres & Diameter of the main screw, m - 32.0.   Diameter of the second screw, m - 7.61.  

Weight of the helicopter: The maximal take-off weight, kg - 56000 Weight empty, kg - 28600 Carrying capacity, kg - 20000 Power-plant  2 ТВД Д-136 capacity, h.p. - 11400 

Firm - Progress Летные the data The maximal speed, km/h - 295 Cruiser speed, km/h - 255 Practical ceiling, m - 6500 Static ceiling, m - 1800 The maximal range of flight, km - 800  Перегоночная range of flight, km - 2000

 


Mi-26T fire-fighting version
Helicopter fire-fighting complex with VSU-15 water-discharging device on external sling is designed for:
• extinguishing and localization of fire sources;
• extinguishing and localization of industrial and domestic fires;
• delivery of mobile fire-fighting refilling stations, wheeled and
caterpillar materiel, as well as ground fire-fighting service
troops to remote and hard-to-access areas of fire.
Fire-fighting helicopter complex comprises:
• VSU-15 water-discharging device;
• external sling providing transportation of VSU-15 and water
intake and discharge control;
• global positioning system;
• thermal vision;
• radio means for communication of crew with ground firefighting
units;
• chemical adds dosage system.
The water-discharging device provides water intake in hovering mode from any water reservoirs
including shallow ones. Water intake and discharge control is performed remotely through
operator's control panel. In case of necessity, VSU-15 can be quickly disconnected, and the
helicopter can be used for transportation of personnel and equipment.
Time, saved due to water intake simplification, allows the helicopter to perform more shuttle
flights to fire source.
Main technical data

VSU-15 maximum volume, m3 15,0 VSU-15 regulated volume, m3 7; 8; 9; 10; 12,5; 13,5
Water intake time, m3/ñ 10 Water discharge rate, tons/sec 1
VSU-15 weight, kg 255 Helicopter's flight speed when water discharge,
km/h 0-120
Flight speed with VSU-15 (with water), km/h up to 180 Flight speed with VSU-15 (without water), km/h up to 200
Recommended altitude when fire-fighting, (if
measured from VSU-15), m from 20 to 60
Dimension of watered strip at flight speed of 30
km/h, Í=20 m width/length, m 12,2/125-330




Refueling complex on the base of Mi-26T
Refueling complex is designed for mobile delivery of various fuel
types and lubricants to material basing sites and autonomous aircraft
and ground materiel refueling on ground.
The refueling complex consists of:
• 2 refueling equipment trolleys with fuel tanks;
• pump aggregates;
• control panels;
• trolleys with distribution sleeves and fuel counters.
Main performance of refueling equipment:
Volume of transported fuel 14 040 liters
Volume of transported lubricants 1 040 liters
Transported fuel:
• aviation
• diesel
kerosene T-2, TS-1, RT
types DL, DZ, DA
Fuel distribution rate by one sleeve:
• 4 sleeves of aviation fuel
• 10 sleeves of diesel fuel
up to 300 l/min (through one sleeve)
50...150 l/min (through one sleeve)
Deployment time for distribution to consumers:
• aviation fuel
• diesel fuel
10 min
15 min
Fuel distribution diagram


BUYERS OF RUSSIAN HELICOPTERS SALES

PLEASE READ BELOW

2023 Aug. 19-24 at Ramenskoye Airfield

just south of Moscow

MAKS is an international airshow held at Zhukovsky International Airport,

the home of the Gromov Flight Research Institute in Zhukovsky

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