NEW AW119 Ke KOALA MKII

Year: NEW October 2011. First registered January 2012

Total Time: 20 hours (aprox)

Colour: Metallic Silver

Interior: Beige Leather

Installed Additional Equipment:
6-seat VIP Leather Cabin

NAT Audio/ICS System

Garmin 430 GPS and #2 VHF Com
Cargo Hook 1400kg Provision Kit
Bambi Bucket Provisions

Upgraded Avionics including NAT Audio/ICS

Garmin GNS420 GPS/Comm

TOTAL PURCHASE PRICE:  US$3,450,000 (excluding VAT/GST)

*Basic AW119Ke Helicopter
AW119Ke with Passenger Cabin Sliding Doors, Equipped with Pratt and WhitneyPT6-B37A Engine, 

*Standard Additional Equipment
– Cabin Fire extinguisher
– Crew Open Door Actuators
– First Aid Kit 
– Pilot/copilot shoulder harness with inertial reel
– Quick disconnecting Chip Detectors
– Baggage Compartment Light
– Tail Boom Strake
– Fuel Drain Electrical Valves
– Pilot headsets (qty 2)
– Radio Master Switch
– 27 Ah Battery (in lieu of 22 Ah battery)

* VFR Avionics Package
– VHF-COM/GPS   Garmin 430
– Moving Map Garmin GMX200
– #2 VHF Comm ICOM
– ICS Cabin/Pilot/Co-Pilot
– Gyrocompass   Honeywell C14A
– Pilot navigation instruments including the following instruments or equivalent:
* ADI
* HSI
– Transponder   KT 70 Mode (S)

* Additional Installed Avionic Equipment 
– AFCS 3 Axis Duplex (Honeywell SP711)
– AC system (2 inverters)
– Garmin 430

* Additional Utility Equipment
– Rotor brake
– Pilot and copilot reinforced windshield
– Pilot and copilot windshield wipers
– Baggage compartment extension (2.1 m)

* Interior and Comfort
– Heater Bleed Air
– Primer finishing cabin walls
– Vibration Dampers Installation

* Miscellaneous
– Air intake/exhaust covers
– Pitot tubes covers
– Ground tools kit including:

• Tie-down fitting provisions
• Tow bar
• Lifting tool
• Ground handling wheels

– Flight Manual and Technical Publications

* Airframe
– Aluminum alloy and bonded panel fuselage
– Semimonocoque aluminum alloy tail boom
– New reinforced skid type landing gear
– Two Jettisonable crew doors (LH & RH)
– Two passenger sliding doors (LH & RH) with jettisonable window
– Acrylic windshield and side windows
– Acrylic overhead windows
– Removable fiberglass tail rotor gear box fairing
– Quick removable tail rotor drive shaft cover
– Separate baggage compartment with hinged door
– Three jacking points
– Removable fairing and cowlings providing 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 metal 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 metal tail rotor hub, teetering, delta-3, hinged type, with two composite material 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
– Dynamic flapping lock mechanism

* Power Plant & Fuel System
– Pratt & Whitney PT6-B37A turboshaft 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
– RH refueling point
– Fuel system control panel
– Three fuel cells (605 lt)
– Submerged fuel pumps (2 boost & 1 transfer  pump)

* Transmission Drive System
– 900 SHP for take off and continuous operation main transmission
– Two stage transmission
– Two transmission mounted hydraulic pumps 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 (engine to main transmission, engine to tail transmission, transmission to blower)

* Electrical
– 28 volt DC 22 Ah nickel cadmium battery with temperature probe
– 200 Ampere self cooled starter generator
– Voltage regulator
– Battery relay
– Interconnecting bus relay
– External power relay
– Distribution buses (2)
– External power receptacle
– Position lights
– 250W landing lights (2)
– Utility lights (2)
– Anti collision lights (2)
– Instrument lights with dimming knob

* Flight Instruments - Pilot
– Barometric encoding altimeter
– Air speed indicator
– Vertical speed indicator
– Magnetic compass indicator
– Clock, 8 days and elapsed time
– Dual tachometer backup instrument

*Instrumentation (on IDS display)
– Inter Turbine Gas Temperature (ITT °C)
– Engine Torque (TQ %)
– Compressor Speed (N. 1 %)
– Turbine Speed (N. 2 %)
– Rotor Speed (NR %)
– Engine Oil Pressure (PSI) and Temperature (°C)
– Transmission Oil Pressure (PSI) and Temperature (°C)
– Fuel Pressure (PSI) and Fuel Quantity (KG)
– Hydraulic pressure (PSI) system 1 & 2
– DC current (Amp)
– DC voltage (VDC)
– AC voltages (VAC 1 & 2)

* Warning, Caution, Advisory  and Maintenance system
– Master warning lights
– Master caution lights
– Aural warning generator 

* Interior Arrangement
– Two individual pilot seats, fore and aft adjustable, with lap belts
– Aluminum alloy honeycomb reinforced floor with anti skid finish
– Ventilation ram air inlets
– Anti reflection instrument panel

* Exterior Finishing
– Finishing in accordance with manufacturer specification NTA893A
– Primer exterior painting