2018 Agusta AW119Kx for sale,

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2018 agusta aw119kx inflight
Make offer
Asia
Year
2018
S/N
14953
Reg
-
TT
250

Aircraft Description

  • EMS Configuration / 2+8 Seating Convertible
  • Single Pilot VFR Configuration (FAA/EASA Standard)
  • MTOW Load 2850kg Internal, 3150kg External
  • Single Stretcher - Removable Parts
  • Air Conditioning
  • 188 Gal Fuel System Upgrade
  • Oxygen Bottle in Baggage Compartment
  • Two Hinged Jettisonable Crew Doors & Two Sliding Passenger Doors
  • Garmin G1000H Integrated Flight Deck System

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Asian Sky Group
  • AIRFRAME / ENGINES / APU / WEIGHT / TOTAL TIME / TOTAL LANDING

    AIRFRAME

    Aluminium alloy and bonded panel fuselage
    Semi-monocoque aluminium alloy tail boom
    New reinforced skid type landing gear
    Two hinged jettisonable crew doors (LH & RH)
    Two sliding passenger doors (LH and RH), 1.10 m opening, with jettisonable windows
    Passenger short foot step (LH & RH)
    Acrylic windshield and side windows
    Overhead cockpit transparent windows
    Lower cockpit transparent windows
    Removable fibreglass tail rotor gearbox fairing
    Quick removable tail rotor drive shaft cover
    Separate baggage compartment with hinged door
    Three jacking points
    Removable fairing and cowlings, for complete accessibility to the controls and drive components
    Quick opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points
    Grounding point

    ENGINES

    Engines Model: PT6B-37A
    Total Hours: 250 Since New

    TOTAL TIME

    250
  • AVIONICS & CONNECTIVITY
    Garmin G1000H Integrated Flight Deck system comprising:
    Two GDU-1040 10.4" display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating:
    Radio tuning controls
    Flight Management System (FMS)
    Synthetic Vision System
    Helicopter Terrain Awareness and Warning System (HTAWS)
    Two GEA-71H Aircraft Interface Unit with integral Central Maintenance Computer (CMC)
    Two GSC-46 Signal Conditioners
    GRS-77H AHRS
    GDC-74H Air Data Computer (ADC)
    Two GIA-63H Integrated Avionics Units (IAU) comprising: COM 1&2 / NAV 1&2 / GPS 1&2 / Aural Alert Generator / DME tuning interface
    GTX-33H Mode-S Transponder with Extended Squitter (ES) capability
    Radar Altimeter RA-4500 FreeFlight Systems
    Digital Audio Control System (DACS) NAT with two cockpit panels
    Magnetic Compass indicator
    L3 Avionics System ESI-2000 Electronic Standby Indicator
    Airframe Hour meter
  • Interior & Entertainment
    Pilot and co-pilot seats, fore and aft adjustable, with lap belts and headrests
    Aluminium alloy honeycomb reinforced floor with anti-skid finishing
    Ventilation ram air inlets
    Anti reflection instrument panel
  • EXTERIOR
    Finishing in accordance with manufacturer specification (NTA893A)
    Primer exterior painting
  • Additional Equipment & Information
    Transmission drive system & hydraulic system
    917 shp for takeoff and 900 shp continuous operation main transmission
    Two-stage transmission
    Transmission mounted hydraulic pumps (2) with separate reservoir
    Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter
    Transmission oil chip detectors (2)
    Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detector
    Transmission cooling and lubrication system
    Transmission shafts

    Rotors and Controls
    Titanium main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite material blades, swept tips, and dampers
    Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite blades, individually interchangeable
    Cyclic and collective controls powered by two hydraulic systems
    Hydraulically powered anti-torque system
    Adjustable friction devices on cyclic and collective system
    Force trim and artificial feel system
    Adjustable directional control pedals
    Flapping and droop restraint mechanism

    Electrical Systems
    28 V DC 22 Ah nickel-cadmium battery with temperature probe
    200 A self-cooled starter generator
    Voltage regulator
    Battery relay
    Interconnecting bus relay
    External power relay
    Distribution buses (2)
    External power receptacle
    Position lights
    250 W landing lights (2)
    Anti collision lights (2)
    Cockpit utility lights (2)
    Instrument lights with dimming switch
    Radio master switch

    Central Warning System (CWS)
    Master warning lights
    Master caution lights
    Warning, caution and advisory messages on PDF display
    Aural alerts from IAU 1 & 2

    System Data (On MFD/PFD)
    Inter turbine gas temperature indicator (ITT°C)
    Engine torque indicator (TQ%)
    Compressor speed indicator (N1%)
    Turbine speed indicator (N2%)
    Rotor speed indicator (NR%)
    Transmission oil pressure (PSI) and temperature (°C) indicator (on MFD)
    Engine oil pressure (PSI) and temperature (°C) indicator (on MFD)
    Fuel pressure (PSI) (on MFD) and fuel quantity (kg) indicator (on PFD/MFD)
    Two hydraulic pressure system indicators (PSI) (on MFD)
    Outside air temperature indicator (°C) (on PFD)
    DC voltmeter (VDC) (on MFD)
    DC ammeter (Amp) (on MFD)

    Ground Equipment
    Air intake/exhaust covers
    Ground tools kit (including tow bar, ground wheels, lifting tool)
    Pitot tube cover
    Rotorcraft Flight Manual (RFM) and technical publications
    Tie-down fitting (main rotor and tail rotor retention straps)

    WiFi

    No

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