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WE HAVE FOR SALE 2012
MI-14 PZH HELICOPTER (AMPHIBIAN)
Oil platforms, coastal areas, between the islands, fire-fighting.

AVIATION COMPLEX OF SUPPRESSION OF SURFACE FIRES ON THE BASIS OF MI-14 PZH HELICOPTER
2.1. Features of the helicopter`s design
The first variant.
The tank with capacity of 4000 liters is installed inside of the fuselage of the helicopter. The tank fillup is made on hovering mode with the help of two electric pumps located on the end of sleeves. The design of the pump unit allows to withdraw/take water from reservoirs or mountain streams with the depth not less than 0,4 meters. The evacuation of water from container is made by opening of the shutters located in the bottom part of the water tank. The part of a design of the tank is located in a special compartment of the helicopter between caissons-tanks under a floor of a cargo cabin of a fuselage.
Lowering and lifting of the pump unit with sleeves in a reservoir is made for a water fence with the help of electric winch ЛПГ-150 or manual winch БЛ-47. The water fence is made on hovering mode at height of 1,5 -2 meters above the reservoir surface.
The second variant.
There is a possibility of usage of the external water discharging device (EWD)(that is similar to those of Mi-8MTV) at installation of an. The water fence is made by lowering EWD in a reservoir on a hovering mode.
2.2. The main flight operation characteristics of the helicopter
2.2.1. Weight of the empty helicopter 8000 kg
2.2.2. The maximum take-off weight 14000 kg
2.2.3. Capacity of the tank for water 4000 l
2.2.4. The Minimum depth of a reservoir for a water fence 0,4 m
2.2.5. Time of full filling of the onboard tank water
From a reservoir in a hovering mode no more than 2 minutes
2.2.6. Duration full plum of water from the onboard
The tank (shock having merged) no more than 10 sec
2.2.7. Volume of the tank for chemically additive liquid 0,4 m
2.2.8. Time of duration of fire extinguishing without refuelling:
- if not used the capacity of the tank of 4000 l up to 1,5 hours.
- if not used the capacity of the tank of 3000 l not less than 3 hours.
2.3. Resources and service life
2.3.1. Initial (between-overhauls) - 1000 hours and 8 years with possibility of prolongation up to 1500 hours.
2.3.2. Assigned - 5000 hours
2.3.3. The assigned service life of Mi-14PZH helicopter – according to the technical condition (assigned service life of Mi-8MTV-1 and Mi-8AMT helicopters and their modifications is 30 years).
2.3.4. The Certificate of Airworthiness is issued under the Type Certificate of Mi-14PZH helicopter of the Aviation Authorities of Ukraine.
***
The price of Mi-14 PZH helicopter:
- with TV3-117VM engines of 02 series – $US4,950 000 US dollars;
- with overhauled modernized engines TV3-117VMA-CBM1V - $US 5 600 000 US dollars;
- with new TV3-117VMA-CBM1V engines– $US 6,100 000 US dollars.
The terms of delivery: FCA – Ukraine (according to Incoterms 2010).
The terms of payment: 50% of advance payment is executed after the inspection of the helicopter at the Aircraft overhaul plant and the rest 50% - when the helicopter is ready after the overhaul.
The time of delivery: the first helicopter will be delivered within 120 days and each subsequent helicopter – within 30 days.

Table No.1.
Comparative flight operation characteristics
of
Mi-14 PZH helicopter
and
Mi-17, Mi-8MТV-1, Mi-171, Mi-172 helicopters.
|
MI-14 PZH |
Mi-8MTV-1, Mi-171, Mi-172 |
Mi-17 |
Crew |
3 |
3 |
3 |
Number of passengers |
24 |
24 |
24 |
Type of engines |
ТV3-117VМ of 02 series or TV3-117VMA-SBM1V |
ТV3-117VМ (VMA) of 02 series |
ТВ3-117МT |
Type of APU |
Аi-9V |
Аi-9V |
Аi-9 |
Type of the main gearbox |
VR-14 |
VR-14 |
VR-14 |
Capacity of the engine (h.p.) |
2 х 2200/ 2 x 2500 |
2 х 2200 |
2 х 2000 |
Weight of the empty helicopter (kg.) |
8000 |
7800 |
7800 |
The maximum take-off weight (kg.) |
14000 |
13000 |
13000 |
The weight of cargo transported in a cabin (kg.) |
4000 |
4000 |
4000 |
The weight of cargo transported on an external cargo sling (kg.) |
4 000 |
4 000 |
3000 |
The maximum flying speed (km./hour) |
250 |
250 |
250 |
Service ceiling (m.) |
6000/9000 |
6000 |
4000 |
Fuel tank capacity (l.) |
3795
(With an additional fuel tank 4595) |
2600*
(With one additional fuel tank 3500 and with two - 4400) |
3795
(With one additional fuel tank 3500 and with two - 4400) |
The landing gear |
The retractable landing gear.
There is a possibility of landing on land and water surfaces. |
The non retractable land gear .
There is a possibility of landing on land surface only. |
The non-retractable landing gear.
There is a possibility of landing on land surface only. |
The documentation |
The Type Certificate of Mi-14PZH helicopter issued by the Aviation Authorities of Ukraine (2010 year) |
The Certificate of Airworthiness of Mi-8MTV helicopter for operation (dd 17.07.1991) |
The Addition to the Certificate of the flight validity of helicopter Mi-8MTV dd 24.08.2001 |
There is a place for installation of an additional fuel tank (on helicopters of transportation type) with capacity of 800 l., which increases the flying range.

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