1976 - Мил Ми-10К Вертолет за Продажба

1976 - Mil Mi-10K Helicopter for Sale 

General description:
The Mil Mi-10 (NATO reporting name Harke), given the product number izdeliye 60, was a Soviet military transport helicopter of flying crane configuration.

Location: USSR (Free Carrier, without VAT)
Year of construction: 1976
Total time (TTAF) TTSN: **** TT
Country: USSR, outside Europe

Specifications:
Crew: 3 people ( 2 pilots and borttehnik ) .
Load capacity : average : 12,000 lbs. , Maximum : 15 000 kg (due to the weight of fuel ) .
Load on the suspension : 8,000 kg .
Inside the fuselage : 3000 kg.
Length : 41.89 m
Fuselage length : 32,86 m
Main rotor diameter : 35.0 m
Tail rotor diameter : 6,3 m
The maximum width of the fuselage : 3.0 m
Height: 9.9 m (with tail rotor stopped ) .
The area swept rotor : 962 m2.
Wheelbase : 8,285 m
 

 

Wheel track : 7.55 m
The distance from the ground to the bottom of the fuselage ( clearance ) : 3.73 m
Empty weight: 27,100 kg .
Normal take-off weight: 38,000 kg .
Maximum Takeoff Weight: 43,550 lbs.
The amount of fuel in internal tanks : 8230 kg (maximum).
Fuel capacity : 10,620 l .
Powerplant : 2 × HPT D-25V .
Engine power: 2 × 5500 liters. s. (2 × 4100 kW).
The plant manufacturer : № *** Plant of Civil Aviation ( Rostov-on- Don) .
For information about accidents : Accidents and incidents flight had.
Location : USSR .
Storage: Enjoy the outdoors on a concrete platform .
Number of passengers: 28 people . , 3 - ton cargo / 65 pers . , Up to 80 people.
Cargo hold : 15.95 * 1.86 * 2.75 - length, width , height.
Range with maximum payload and maximum fuel capacity : 500 km .
Class aerodrome runways - 120 by 60 meters.
Fuel type: kerosene TS - 1, T - 1.
Flow characteristics : Kerosene - 2300kg/chas . , Oil - 300 kg / year

 

Performance:
Maximum speed: 235 km / h
Cruising speed:
When the mass of 38000 kg and less than 220 km / h
When the mass of over 38,000 kg: 180 km / h
Operational range : 250 km .
Flight duration: 1 h 30 m
Ferry range : 695 km .
Flight duration: 3 h 45 m
Service ceiling : 3,000 m
Rate of climb : 6.3 m / s . (maximum).

The composition of airborne navigation equipment and communications :
VHF p / st . " Cormorant - 20 » № 1.
VHF p / st . " Cormorant - 20 » № 2 .
KV p / st . " Carat" .
Automatic Direction Finder : ARC - 9.
P / altimeter: PB - 3.
Defendant: 020 M.
Player: MS - 61.
Onboard flight data recorder , the system : MSRP - 12 - 96.
Defendant secondary location : CT - 76A , with a height sensor AK - 350 .
Satellite Navigation System : GPS - 95 .
Automatic Direction Finder VHF : ARC - U2 .
Compass system : MMC - 1A.
Autopilot: AP - 34B .
Altimeter : HP - 10K .

Guidance system :
Locking swivel with vezoizmeritelnym device.
Castle podtsepka .
Cable Set .
Hydraulic unit : GB - 1.

The composition and characteristics of the equipment :
The composition and characteristics of cargo equipment : LPG winch - 3. Transporter .