2015 СЛЕД КАПИТАЛЕН РЕМОНТ МИЛ Ми-14 {Капитален ремонт 2015, по контракт, с EC гаранция} за Продажба

2015 REBUILT MIL Mi-14 {Complete overhaul 2015, on contract} for Sale  

General description:
Multifunctional, export configuration brand new with additional equipment  carrying passengers and cargo
transportation of bulky cargo on the external load search and rescue operation medical evacuation

Location: Bulgaria
Year of construction: 1980-82, Rebuilt 2015 (three - four months of advance payment, Aviation factories with all license)
Total time (TTAF) TTSN: 6000-6500 TT
Country: Bulgaria - 1 pct  and USSR- 3 pct

Condition on the purchase: FCA - Burgas Bulgaria (Free Carrier, free zone BG, without VAT)

General description:
Rebuilt 2015,

Airplane time:  6000-6500 Hrs, after Rebuilt 2015 -  0 Hrs, Life between overhaul: 4500 Hrs; Assigned service life time: 2025

Main Gearbox time: 1980 - 6000-6500 Hrs, after Rebuilt 2015 -  0 Hrs, Life between overhaul: 2500 Hrs; Assigned service life time: 2025

Main Engine time 2xTB3-117BM 02 : 1980-86 - 1600-1920 Hrs, after Rebuilt 2015 -  0 Hrs, Life between overhaul: 2580 Hrs;  Assigned service life time: 2025

Interior: Standard grey.

Exterior: White or other colors

Avionics: Avionics standard that was on the Mi-14 helicopters:

1.2. The main geometrical data

1.2.1.   Length of the helicopter                     18374 mm
1.2.2.   Height of the helicopter                      5332 mm
1.2.3.   Diameter of the main rotor                 21294 mm
1.2.4.   Diameter of the tail rotor                    3908 mm

1.3. The weight and balance data
1.3.1. Take-off weight:
-           Normal                        13000 kg
-           Maximum                    14000 kg
1.3.2. Maximum-permissible heaviness with respect to a rotor shaft axis is:
-           bow heaviness             + 300 mm (ahead of a rotor shaft axis)
-           tail heaviness               + 30 mm   (ahead of a rotor shaft axis)

1.4. Capacity of fuel tanks
1.4.1.   Fuel-consumed tank l/kg         445/346
1.4.2.   Boat l/kg                                 3350/2600
1.4.3.  The general capacity of l/kg     3795/2946

1.5. The main flight operation characteristics of the helicopter
1.5.1. The maximum instrument speed:
-G NORMS. = 13000кг                     230km/hour
-G max. = 14000кг                             220km/hour
1.5.2. Cruiser speed of flight:
210 km/hour
205 km/hour
1.5.3. Economic indicated air speed
At G norm. and G max.                      130km/hour
1.5.4. Service ceiling:
-G norm. = 13000 kg                          3600m.
-G max. = 14000kg                             3100m.
1.5.5. Operational range of flight:
- G norm. = 13000kg                          970km.
- G max. = 14000кг                            930km.