1993_Eurocopter_BK-117-B2_7247

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    This airc raft is sold by:

    Savback Helicopters AB

    Contact person: Michael Savback

    Contact phone: +46706365135

    Email: [email protected]

    Website: www.savback.se

    Made year:1993 Manufacturer:Eurocopter Model:BK 117 B-2

    ManufacturerEurocopter

    ModelBK 117 B-2

    Made year1993

    SN7247

    Reg. no.TBD

    LocationGermany

    Price3.4 M EUR

    General details:

    4726 hours TT. EMS or VIP configuration. No damage history. Engine overhaul performed in December 2010, main gear box installed in January 2011 together

    with floatation system.

    Detailed description:

    TTSN: 4726 hours TSN

    ENGINE SYSTEM:

    Two Lycoming engines, model LTS101-750B-1

    Engine fire extinguishing system

    Fuel system in flexible bladder tanks

    Oil cooling and lubricant system

    WING UNIT:

    Jointless main rotor ''Blkow Sys tem''

    Four GFK rotor blades with erosion protection

    Titanium rotor head

    Transmission as sy, Kawas aki KB03

    Two independent oil cooling and lubricant systems

    Rotor brake

    Dynamic vibration absorber

    TAIL ROTOR:

    Two-blade ro tor (semi-rigid)

    Two wrapped GFK ro tor blades with eros ion protection

    http://www.savback.se/
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    CELL:

    Two folding cockpit doors with emergency e ject mechanism, vent windows and card pockets

    Two sliding doo rs with emergency e ject mechanisms

    Two folding cargo hold doors, rear

    Landing gear runners with runner protection and continuous boarding steps

    Maintenance steps and handles

    Single control with tandem hydraulics for main rotor control

    Electrical trim system, lengthwise and crosswise

    Driving dynamics regulator

    Steering reversal prevention system (SPAS)

    Tail boom with rigid height and vertical stabiliser including winglets

    Tail skid

    Paintwork (see photo)

    COCKPIT AND CABIN EQUIPMENT:

    Height and lenght-adjustable pilot and co-pilot seats with headrests, adjustable lap and shoulder belts with automatic belt locking

    Padded bench seats

    Interior cladding with soundproofing

    Floor covering for cockpit, cabin, cargo hold

    Dust ventilation and electrical ventilation system

    Ceiling lighting in cockpit and cabin

    Lashing eyes in cabin and cargo hold floor

    Inspection lamp fed by the vehicle electrical system in the cockpit

    Two portable fire extinguishers

    Baton torch

    Windscreen wipers (pilot and co-pilot side)

    Card pockets on the instrument panel visor and on the left and right of the central console

    Holder for audio headsets

    ELECTRICAL SYSTEM:

    Two starter generators (2 x 150 A /28V DC)

    Nickel-cadmium battery, 24 V, 25 Ah (20cells), Varta

    Precaution for outboard power supply

    Outlet for inboard power supply

    Voltmeter, dual

    Ammeter, dual

    Pitot tube and openings of the static pressure measuring system heated

    Position and co llision warning lights (red rotating light)

    Landing lights, rigid

    Searchinglights, rotating

    AC converter

    AVIONICS:

    Flight InstrumentsAirspeed indicator

    Coded altimeter (see radio/nav. equipment)

    Instantaneous variometer

    4 artificial horizon

    3 artificial horizon, Narco AIM 510-1G (see radio/nav. equipment)

    Directional gyro

    Magnetic compass

    External thermometer

    On-board clock

    ENGINE INSTRUMENTS AND DISPLAU EQUIPMENT:

    Triple tachometer for rotor and engines (N2)

    Two tachometers for engines (N1)

    Two displays for exhaust gas tempera ture (TOT)

    Douple torque display

    Two displays for engine oil pressure and temperature

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    Double display for gear oil pressure

    Display equipment for gear oil temerature

    Triple fuel rese rve display

    Two displays for hydraulic pres sure

    Operating hours counter

    Warning Lights and Information Systems

    Warning light display panel

    Two main warning lights

    Engine fire warning display

    Mast torque display

    Acoustic warning for rotor and engine s peed

    INTERIOR:

    EMS or VIP

    EXTERIOR:

    Red and Yellow

    MAINTENANCE:

    No damage history. Engine overhaul performed in December 2010, Main Gear box is being installed in Jan 2011 along with a flotation system.

    NOTES:

    The aircraft is operating, why the condition and component times will be subject to changes depending upon such operations. Verification of the condition of

    the aircraft and its component times shall be be the responsibility of the purchaser.