AgustaWestland AW119kx I-EUKX

For sale


Manufacturer: Leonardo

Aircraft type: Aw119MkII (KX)

Aircraft registration: I-EUKX

S/n: 14918

Year:  2016

T.T.:  140 h

Engine type:  PW PT6B-37b

Engine S/n: PCE-PUC2744

T.T.: 140 h

T.S.O: 0 h

C.S.N: 150 cy




1.1. 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), 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 points

1.2. 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

1.3. Power Plant and Fuel System


  • Pratt & Whitney Canada PT6B-37A turbo-shaft engine
  • Engine mounted fuel pump and filter assembly
  • Engine mounted oil pump and filter assembly
  • Engine mounted fuel control and governor
  • Electronic Engine Control (EEC)
  • Lubrication and cooling system
  • Engine oil chip detector (1)
  • Engine mounted fuel heater
  • Fuel system control panel
  • 3-cell fuel system (605 l – 160 US gal)
  • Submerged fuel pumps (2 boost and 1 transfer pump)
  • RH refuelling point

1.4.  Transmission / Drive System and Hydraulic System


  • 917 shp for take-off 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

1.5. Electrical System


  • 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 (NVG compatible)
  • 250 W landing lights (2)
  • Anti-collision lights (2) (NVG compatible)
  • Cockpit utility lights (2) (NVG compatible)
  • Instrument lights
  • Radio master switch

1.6. Avionic Package


Depending on both contractual delivery date and Country of destination, the AW119Kx helicopter could be delivered with EASA/FAA Type Certification or could be equipped with Garmin G1000HTM approved as FAA STC.

The latter does not include the magnetic compass indicator.

  • Garmin G1000HTM Integrated Flight Deck system comprising:
    • Two GDU-1040 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
    • 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
      • ADF interface
      • DME tuning interface
    • GTX-33H Mode-S Transponder with Extended Squitter (ES) capability
  • Radar Altimeter RA-4500 FreeFlight Systems
  • Digital Audio Control System (DACS) COBHAM with two cockpit panels
  • Magnetic Compass indicator
  • L3 Avionics System ESI-2000 Electronic Standby Indicator
  • Engine Hour meter

1.7. Systems Data (on PFD/MFD)


  • 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)

1.8. Central Warning System (CWS)


  • Master warning lights
  • Master caution lights
  • Warning, caution and advisory messages on PFD display
  • Aural alerts from IAU 1 & 2

1.9. Interior Arrangement


  • 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

1.10. Exterior Finishing


  • Finishing in accordance with manufacturer specification

1.11. Miscellaneous / Ground Equipment


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



2.1. Standard Equipment


  • 28 Ah battery (in lieu of 22 Ah battery)
  • Active Noise Reduction (ANR) headsets (pilot and co-pilot)
  • Baggage compartment lights
  • Crew open door actuators
  • First aid kit
  • Fuel drain electrical valves
  • Portable fire extinguisher
  • Quick disconnecting chip detectors
  • Shoulder harness with inertial reels (pilot and co-pilot)
  • Tail boom strake

2.2. Additional Avionic Equipment


  • AC power supply system (2 inverters)
  • AFCS 3-axis duplex SP-711 Honeywell

2.3. Additional Equipment


  • Baggage compartment extension (1.9 m)

(*) It may be affected by avionic customization

  • Dual controls
  • Fuel cap with key-lock
  • Reinforced windshields (pilot and co-pilot)
  • Rotor brake
  • Sliding windows on cockpit doors
  • Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
  • Interior Trim


  • Bleed air heater
  • Primer finished cabin walls



3.1.  Interior Equipment - Cabin


  • VIP interior - 6 places
    • Soundproofing
    • Leatherette covered liners
    • Seats covered with leather
    • 3 aft facing seats (central bench)
    • 3 facing seats (aft bench)
    • 3-point shoulder harness with inertial reels and safety belts for all passenger seats
    • Reading lights, advisory lights
    • Cabin loudspeakers
    • Headset Bose ANR type (Qty 6)
    • Floor carpeting

3.2. Cabin Interior Equipment


  • Leather covering for 6 passenger seats with armrest

3.3.  Utility Equipment


  • Air conditioning
  • 230 US gal fuel system (in lieu of 160 US gal)
  • High visibility passengers’ doors
  • Pilot and co-pilot pedal extension
  • Pilot multipurpose holder
  • Baggage compartment extension (2.3 m)
  • Cargo hook primary (1400 kg) provision
  • Wire strike protection system
  • Steps Long Boarding D119-675 (LH and RH)
  • Engine inlet barrier filter

3.4.  Finishing - Painting


  • Customised painting scheme


helicopter logo

Are you interested in our services?

We are a reliable partner for helicopter maintenance and a serious and efficient flight school.

Contact us

EUROTECH Helicopter Services
Via Valeriana, 8
23010 Caiolo (SO) Italy

+39 0342 354013

P.IVA 00669210148
REA Sondrio n° 47013
Cap. Soc. int. vers. € 80.000

Via Valeriana 8
23010 Caiolo (SO)

Elisuperficie Flytech
N 46° 9' 31" / E 9° 48' 38"

Viale Antonio Gramsci 1
20091 Bresso MI

45°32.5′N 9°12.2′E

Roma Nord Capena
Via di Scorano snc
00060 CAPENA Roma

N 42° 7' 13" / E 12° 36' 6"

© 2023 EUROTECH Helicopter Services | Privacy Policy | Cookie Policy 

| Manage your consents

designed by Pura Comunicazione