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

AW119Kx CONFIGURATION

1.  AW119Kx BASELINE AIRCRAFT

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.  STANDARD AIRCRAFT

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.  I-EUKX OPTIONAL INSTALLED

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