Leonardo AW119Kx

Avionic Package

Avionics Equipment
- 1X-K-070-5CM TAS GTS 800 Garmin

Garmin G1000NXi Integrated Flight Deck system comprising:
- Two (2) GDU-1050H display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating:
• Flight Management System (FMS)
• Synthetic Vision System (SVS)
• Helicopter Terrain Awareness and Warning System (HTAWS)
• Radio tuning controls

- Two (2) GEA-71BH Aircraft Interface Unit
- GRS-7800 AHRS
- GDC-72H Air Data Computer (ADC)
- Two GIA-64H Integrated Avionics Units (IAU) comprising:
• COM 1&2
• NAV 1&2
• GPS 1&2
• Aural Alert Generator
- Transponder GTX-345R Mode-S/ADS-B dual mode 1090 Extended
- Squitter (ES) ADS-B Out plus 1090 and 978 ADS-B In compliant position source (WAAS/GPS)
- Airframe Hour meter
- Central Maintenance Computer (CMC) data logging

- Radar Altimeter GRA-55
- Digital Audio Control System (DACS) COBHAM with two (2) cockpit panels
- Magnetic Compass indicator
- L3 Avionics System EFD 750 Electronic Standby Indicator

- Systems Data (on PFD/MFD)
- Inter turbine gas temperature indicator (ITT°C) (on MFD)
- Power index (on PFD)
- Engine torque indicator (TQ%) (on MFD)
- Compressor speed indicator (N1%) (on MFD)
- Turbine speed indicator (N2%)
- Rotor speed indicator (NR%)
- Transmission oil pressure (PSI) and temperature (°C) indicator
- Engine oil pressure (PSI) and temperature (°C) indicator
- Fuel pressure (PSI) and fuel quantity (kg) indicator
- Two (2) hydraulic pressure system indicators (PSI)
- Outside air temperature indicator (°C) (on PFD)
- DC voltmeter (VDC)
- DC ammeter (Amp)

Central Warning System (CWS)
- Master warning lights
- Master caution lights
- Warning, caution and advisory messages on PFD display
- Aural alerts

Standard Equipment
- 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 (two [2] inverters)
- AFCS 3-axis duplex SP-711 Honeywell
- Emergency Locator Transmitter

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
- Hourmeter (engine run-time)
- Pulsed chip detectors
- In lieu of quick disconnecting chip detectors.

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

Utility Equipment
- 1X-K-151-3CM Air conditioning
- 1X-K-101-6CM 230 USgal fuel system
- In lieu of 160 USgal
- 1X-K-103-6CM Baggage compartment extension (2.3 m)

- 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

Interior Trim
- Bleed air heater
- Primer finished cabin walls

PROPOSED CONFIGURATION
- Interior Equipment - Cabin
- 1X-A-020-3CM VIP interior - 6 places
- Soundproofing
- Leatherette covered liners
- Seats covered with leather
- 3 aft facing seats (central bench)
- 3 fwd 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

- Finishing in accordance with manufacturer specification
- Primer exterior painting

Painting
Standard painting and finishing
- Up to 4 colours from LHD selection
- painting scheme and finishing from LHD selection
- Registration marks and logos (decal)

Finishing - Painting
- 1X-K-001-8CM Customized painting and finishing
- Customized colours
- Customized painting scheme and finishing
- Registration marks and logos

AW119KX VFR BASELINE AIRCRAFT
Airframe:
- Aluminium alloy and bonded panel fuselage
- Semi-monocoque aluminium alloy tail boom
- Reinforced skid type landing gear - black colour
- Two (2) hinged jettisonable crew doors (LH and RH)
- Two (2) sliding passenger doors (LH and RH), 1.10 m opening, with jettisonable windows
- Passenger short foot step (LH and RH)
- Polycarbonate windshield and side azure coloured windows
- Overhead cockpit azure coloured windows
- Lower cockpit azure coloured windows
- Removable composite tail rotor gearbox fairing
- Quick removable tail rotor drive shaft cover
- Separate baggage compartment with hinged door
- Three (3) 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

Rotors and Controls
- Titanium main rotor hub, corrosion protected, fully articulated with four (4) composite grips, four (4) elastomeric bearings, four (4) individually interchangeable composite material blades, swept tips, and dampers
- Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two (2) composite blades, individually interchangeable
- Cyclic and collective controls powered by two (2) 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

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
- One (1) engine oil chip detector
- Engine mounted fuel heater
- Fuel system control panel
- 3-cell crash-resistant fuel system
- Submerged fuel pumps (two [2] boost and one [1] transfer pump)
- RH refuelling point

Transmission / Drive System and Hydraulic System
- 917 shp for take-off and 900 shp continuous operation main transmission
- 2-stage transmission
- Two (2) transmission mounted hydraulic pumps with separate reservoir
-Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter
- Two (2) transmission oil chip detectors
- 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 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
- Two (2) LED landing lights
- Two (2) anti-collision lights
- Two (2) cockpit utility lights
- Instrument lights
- Radio master switch