2023 Leonardo AW119 Kx Koala Enhanced

TTAF: 15.5

Landings: 64

US C of A issued June 24, 2024

Aluminiumalloy and bonded panel fuselage

Semi-monocoque aluminiumalloy 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

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

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

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

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

• 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

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)

AC power supply system (two [2] inverters)

AFCS 3-axis duplex SP-711 Honeywell

Emergency Locator Transmitter

Pilot and co-pilot seats, fore and aft adjustable, with lap belts and headrests

Aluminiumalloy honeycomb reinforced floor with anti-skid finishing

Ventilation ram air inlets

Anti-reflection instrument panel

AC power supply system (two [2] inverters)

AFCS 3-axis duplex SP-711 Honeywell

Emergency Locator Transmitter

Bleed air heater

Primer finished cabin walls

Finishing in accordance with manufacturer specification

Primer exterior painting

Standard painting and finishing

Up to 4 colours from LHD selection

painting scheme and finishing from LHD selection

Registration marks and logos (decal)

Warranty Commencement Date June 24, 2024

Warranty Expiration Date June 23, 2027 (or 2,000 Hours)

No Damage / No Incidents