2016 Airbus H130 For Sale, Turkey

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Airbus H130 1
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Airbus H130 2
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Airbus H130 3
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Airbus H130 4
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Airbus H130 5
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Airbus H130 6
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Airbus H130 7
Please call
Europe, Turkey
Year
2016
S/N
8220
Reg
TC-HSG
TT
580

Aircraft Highlights

Fresh 48mo inspection 
Tail boom Modification complied with

  • H130 Baseline Aircraft
  • VFR day and night package with integrated Garmin 750H, included in baseline definition
  • First Aid Kit - Stylence® layout
  • Engine flushing device without removal of cowlings
  • Enhanced Engine Air Particle Separator
  • Tinted windows for front windscreens
  • Sun protected upper windows
  • Dual controls
  • Enhanced Air conditioning system
  • Cargo Sling (1500kg) Fixed Parts
  • Emergency Floatation Gear - Fixed and removable parts
  • Stylence Layout

Seat Color: Brown CL332                                           
Carpet, Argent: Louisiane range     
Ceiling and partition panels TAPIS ultra-suede: Coffee bean 3147     
Cyclic, collective, ventilation outlets and cabin lights are leather upholstered in   harmony with seats

  • ICS installation compatible with Bose headset
  • Bose headset (x7)
  • Radio altimeter Thales AHV16, instead of Turn and Bank indicator
  • Stand-by gyro horizon Thales H321EGM

 

 

Read More
Europlane Aviation Services
  • AIRFRAME / ENGINES / APU / WEIGHT / TOTAL TIME / TOTAL LANDING

    AIRFRAME

    Enrolled on CAMP
    Engine Model : Turbomeca Arriel 2D
    TSN : 580 hrs
    CYC : 1991

    TOTAL TIME

    580
  • Additional Equipment & Information
    COCKPIT AND CABIN
    • Cabin floor in light-alloy sheet-metal
    • 1 pilot high-back energy-absorbing seat, adjustable in reach, removable, complete with cushions, safety belts and shoulder harnesses
    • 6 passengers high-back energy-absorbing seats, removable, complete with cushions safety belts and shoulder harnesses:
    • 2 front right, including for 1 copilot (copilot controls are optional)
    • 4 rear row
    • 2 cockpit jettisonable hinged doors
    • 1 LH front door fitted with a sliding window
    • 1 RH front door compatible with 8 seat layout
    • 1 LH rear sliding door
    • 1 RH rear sliding door
    • Locks on every access to cabin and luggage compartments
    • Lock on fuel cap
    • Lateral and upper tinted windows (windscreen excluded)
    • 1 ceiling housing the cabin lighting, 7 air ventilation outlets and controls (rotor brake and fuel cut-off)
    • Dynamic ventilation system
    • Cabin heating
    • Demisting system for front windscreens
    • 2 pilot document holders
    • Door map case in LH and RH front doors
    • Rear bulkhead and lateral rear upholstery
    • 1 fire-extinguisher
    • 1 Flight Manual in English



    INSTRUMENTS
    • 1 airspeed indicator
    • 1 altimeter
    • 1 vertical speed indicator
    • 1 LCD dual RPM tachometer (rotor and free turbine)
    • 1 stop watch
    • 1 warning panel
    • 1 magnetic compass
    • 1 heated pitot head
    • 1 external side slip indicator
    • 1 control box for light and electrical generation
    • 1 ICS connection to audio warning issued from VEMD®
    • 1 cockpit imaging and flight data monitoring device
    • 1 LCD dual screen Vehicle and Engine Multifunction Display {VEMD) providing the following information:
    • First Limit Indicators {FLI)
    • Torquemeter
    • Exhaust gas temperature (TOT)
    • Gas generator tachometer (N1)
    • Engine oil temperature, pressure
    • Fuel quantity
    • Fuel flow and estimated remaining time to fly
    • Ammeter and voltmeter and battery temperature
    • Outside Air Temperature {OAT)
    • Enhanced usage monitoring functions
    • IGE/OGE performance calculations
    • Engine cycles counting
    • Engine power check
    • Overlimits display
    • VEMD and peripheral maintenance information
    • Data downloading capability (software and connection wire as option)

    AVIONICS
    • Avionics master switch
    • 1 gyro-horizon
    • 1 gyro-compass with
    • 1 horizontal Situation Indicator
    • 1 turn and bank indicator
    • 1 VHF/VOR/LOC/GS
    • 1 VHF/VOR/LOC/GS/GPS
    • 1 transponder (mode S)
    • 1 altitude encoder
    • 1 Emergency Locator Transmitter
    • 1 ICS + passenger interphone

    POWER PLANT
    • 1 Turbomeca ARRI EL 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 back-up fuel control box that automatically controls the engine in case of a total failure of the 2 digital channels of the FADEC
    • 1 crashworthy fuel system including 1 tank of 540 liters (143 US gal.) total capacity
    • 1 twist grip on pilot side (for engine reduction in case of tail rotor failure and autorotation training)
    • 1 magnetic plug and 1 chip detector
    • 1 engine lubrication and oil cooling system
    • 1 fire detection system
    • 1 air-intake protection grids
    • 1 torque-measurement pick-up

    TRANSMISSION SYSTEM
    • 1 main gearbox, anti-vibration mounted, with oil sight gauge, chip detector, oil temperature and pressure switches, port for endoscope and self sealing valve for oil sampling and draining
    • 1 main gearbox oil cooling system
    • 1 engine to main gearbox coupling shaft
    • 1 rotor brake
    • 1 main rotor high and low rpm warning device
    • 1 tail drive carried by five anti-friction bearings
    • 1 tail gearbox with oil sight gauge, chip detector and port for endoscopic inspection

    ROTORS AND FLIGHT CONTROLS
    • 1 main rotor with 3 composite-material blades around a STARFLEX® head fitted with spherical thrust bearings
    • 1 anti-torque rotor (FENESTRON) with 10 asymmetrical blades, integrated in vertical fin
    • 3 main rotor hydraulic servo units (duplex servos)
    • Integrated back-up control valve on each body of each duplex servo

    HYDRAULICS
    • 2 independent hydraulic systems feeding the duplex servos

    ELECTRICAL INSTALLATION
    • One 150 A, 28 VDC starter-generator
    • One 15 A.h cadmium-nickel battery
    • 1 ground power receptacle
    • 3 position lights (LED)
    • 1 flashing anti-collision light (LED)
    • 2 fixed landing lights
    • 2 cabin light sets, each with 2 reading lights for 2 rear passengers and 1 dome light
    • 1 integrated instrument panel lighting system
    • Integrated lighting in central console
    • 1 reading map light on upper canopy strut for pilot
    • 1 cockpit breaker panel
    • One 28 V DC cabin power outlet

    AIRBORNE KIT (weight not included in the baseline aircraft empty weight)
    • 1 pitot head cover
    • 2 static port stoppers
    • 1 engine air-intake blanking cover
    • 1 exhaust pipe blank
    • 2 hydraulic ground handling bogies
    • 1 cargo net and rope
    • 1 lifting ring
    • 2 upper mooring rings
    • 3 main-blade socks and pole
    • 1 document holder
    • 1 airborne kit stowage bag
    • 1 front air-intake blanking cover
    • 1 fuel tank bleeding
    • 3 ballast plates


    WiFi

    No

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