1965 MIL MI 1
Aircraft Summary
General
Year
1965
Manufacturer
MIL
Model
MI-1
Condition
Used
FlightRules
VFR
Description
Helicopter in working condition. Good condition. Exchange for a Robinson R-44 in the Russian Federation
Airframe
Total Time
1000.0
Airframe Notes
The fuselage has a truss with a shell of aluminum alloy tail boom semi-monocoque construction with the reject end up beam and controlled stabilizer. The cabin located in the front seat pilot and two passengers in the back, in a training version with dual controls - student in the front seat and the instructor behind him
Rotor
Rotor Notes
Rotor - three-bladed, with hinged blades and friction dampers. The blades are mixed with the tubular spar construction made of steel, wood stringers and ribs and a covering made of fabric and plywood. Blades trapezoidal planform and profile 230 NACA variable relative thickness. Recent versions of the Mi-1 were equipped with rectangular, all-metal blades with extruded spar made from aluminum alloy with attachments thereto sections with aluminum, honeycomb. Tail rotor - three-bladed, with a diameter of 2.5 m pushing, with wooden blades trapezoidal shape. [4]
Engine
Engine Notes
The power plant includes one star semitsilindrovy piston engine AI-26B design Ivchenko capacity of 423 kW. It is installed in a horizontal position and is equipped with the bevel gear and a fan for forced cooling. [4] The engine is started with compressed air, the stock of which was small. To avoid falling into a difficult situation, when the air was over, and the engine can not start somewhere in the middle of the taiga, the pilots carried a spare can of compressed air
Modifications/Conversions
Modifications/Conversions
Helicopter in working condition. Raise the 1 per year into the air to keep working. Also there is a lot of spare parts (by almost 2 helicopter, except the fuselage)
Avionics
Avionics/Radios
standard devices
Additional Equipment
Additional Equipment
Special equipment allows the helicopter to fly at any time, even in adverse weather conditions. Main rotor and tail rotor, as well as the windshield of the cockpit equipped with anti-icing systems alcohol.
Exterior
Year Painted
2012
Exterior Notes
The fuselage has a truss with a shell of aluminum alloy tail boom semi-monocoque construction with the reject end up beam and controlled stabilizer
Interior
Year Interior
1965
Number of Seats
3
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