AW119kx I-EUKX – 2016

Aircraft Description

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 cyAW119Kx

CONFIGURATION

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

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 mechanis

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

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

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

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

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)

Central Warning System (CWS)

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

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

Exterior Finishing

Finishing in accordance with manufacturer specification

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)

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

Additional Avionic Equipment

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

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

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

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

Avionic Package

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

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)

Central Warning System (CWS)

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

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

Exterior Finishing

Finishing in accordance with manufacturer specification

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)

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

Cabin Interior Equipment

Leather covering for 6 passenger seats with armrest

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

Finishing - Painting

Customised painting scheme

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

Avionic Package

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