Model AW139
Year of Manufacture 2008
First Registry 2010
Registration Number TC-HKU
Aircraft S/N 41016
TSN 281,44
Engines Pratt & Whitney PT6C S/N PCE KB0347




  • Aluminum alloy fuselage
  • Polycarbonate windshields
  • Overhead cockpit windows
  • Lower cockpit windows
  • Cockpit ram air adjustable outlets
  • Forced fan ventilation
  • Bleed air heater and defroster with air noise suppressions
  • Heated Pitot tubes (2) with pilot heat failure warning (2)
  • Heated static intakes (2)
  • One cockpit and one cabin fire extinguisher
  • Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side)
  • Plugin sliding doors (2) for passenger cabin access with four locking latches
  • Six cabin push-out emergency exit windows (two on each passenger cabin
  • door)
  • Baggage compartment with 2 lockable baggage compartment doors (LH and
  • RH)
  • Baggage compartment cargo tie-down fittings
  • Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear)
  • Structural provisions for nose landing gear doors
  • Landing gear mooring
  • Upper deck mooring provisions
  • Hoisting and jacking fittings
  • Tail boom and vertical fin
  • Stabilizers with composite “winglets”
  • Pilot and co-pilot windshield wipers
  • Maintenance steps for access to upper deck on both sides
  • Upper deck cowlings (one front forward sliding, two side opening for engine access)
  • Steps for cockpit access
  • Anti-vibration masses (2) under cabin floor


  • Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers
  • Rotating M/R flight controls
  • Main rotor hub
  • Main dual servo actuators (3)
  • Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers
  • Rotating T/R flight controls
  • One T/R dual servo actuator
  • Force trim system
  • Pilot fixed flight controls (cyclic, collective, anti-torque pedals)
  • Co-pilot fixed flight controls (cyclic, collective, anti-torque pedals)
  • Dual digital 3-axis linear actuators
  • Rotor brake
  • Provision for main rotor tracking (magnetic pick-up)


  • Two Pratt & Whitney Canada PT6C-67C engines
  • Two magnetic chip detectors
  • Two integrated and independent engine oil coolers
  • Separate firewall protection for each engine
  • Fire detection system
  • Fire extinguisher system (2 bottles)
  • Steel engine exhausts and ejectors
  • Two independent crashworthy fuel cells
  • Two supply pumps on engines
  • Two submerged booster pumps in fuel tank
  • Two fuel filter assemblies
  • Two engine back-up controls, mechanical and electrical
  • Two manual engine start and ignition systems


  • Main transmission with two direct drive engine inputs
  • Three main transmission chip detectors/debris collectors with burning capability
  • Two freewheel units
  • Four strut rods for upper deck attachment and one anti-torque plate
  • Intermediate gearbox with sight gauge and magnetic drain plug/chip detector
  • Tail gearbox with sight gage and magnetic drain plug/chip detector
  • Dual independent, redundant hydraulic systems
  • Two hydraulic Power Control Modules (PCM)
  • Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation
  • One electrical pump for control checks on ground (engines off)
  • Air conditoning compressor quill


  • DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators
  • DC external power receptacle
  • Two nickel-cadmium batteries: one 40 Ah main battery plus one 27 Ah auxiliary battery
  • DC Starter Generator Control Units (2)
  • Navigation lights (3)
  • Anticollision light
  • External emergency landing lights on the sponsons (2)
  • Fixed landing/taxiing lights on the sponsons (2)
  • Retractable/rotating landing light
  • Baggage compartment lights (3) and smoke sensor


  • 1st PFD (Pilot Primary Flight Display 8″ x 10″ color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
  • 2nd PFD (co-pilot Primary Flight Display 8 ” x 10″ coior Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
  • 1st MFD (Pilot Multifunction Display 8″ x 10″ color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
  • 2nd MFD (co-pilot Multifunction Display 8″x 10″ color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
  • One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data)
  • Two Attitude and Heading Reference Systems (AHRS)
  • Two Air Data Modules (ADM)
  • Two flux valves
  • Two Display Controllers (DC)
  • Two Cursor Control Devices (CCD)
  • One Reversion Control Panel (RCP)
  • One Display Dimming Control Panel (DCP)
  • One Stability Augmentation System (SAS) control panel
  • Two Remote Instrument Controllers (RIC)
  • Two Modular Avionic Units (MAU) incorporating the following major subsystems and/or functions:
  • Vehicle Monitoring System (VMS) dual
  • Monitor Warning System (MWS) dual
  • Aural Warning Generator (AWG) single
  • Central Maintenance Computer (CMC) single
  • 4-axis dual Digital Automatic Flight Control System (DAFCS) with autotrim function
  • Provision for CVR/FDR data interface (single)
  • Flight Director System (dual)
  • Pilot and co-pilot microphone and headset
  • Pilot and co-pilot interphone control (cyclic grip and floor switches)
  • Left Modular Radio Cabinet (MRC) wilh the following modules:
    • One VHF Comm.
    • One VOR/LOC/GS/MBz
  • Right Modular Radio Cabinet (MRC) with the following modules:
    • One VHF Comm.
    • One Mode S diversity transponder
    • One VOR/LOC/GS/MB
    • One ADF
    • One DME
  • Two pedestal mounted Multi Control Function Display Units (MCDU)
  • Emergency Locator Transmitter (ELT) – 121.5/243/406 MHz
  • One Flight Guidance Controller
  • Honeywell GPS module with Flight Plan Management System (FPMS)
  • Pilot and co-pilot digital audio panels with remote ICS audio port for ground
  • Pilot clock (digital)
  • co-pliot clock (digital)
  • One magnetic compass
  • One Outside Air Temperature indicator
  • Two Master Warning Lights (MWL)
  • Two Master Caution Lights (MCL)
  • Engine 1 Fire Light
  • Engine 2 Fire Light
  • Baggage compartment smoke detector light
  • Dual electrical power connection for CVR/FDR (FAA/EASA requirement compliant)
  • Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater
  • Locator Beacon (ULB)


  • Pilot and co-pilot crashworthy seats (with inertial reels and safety belts)
  • Cockpit dome/storm light
  • Cockpit utility lights (2)
  • 28V DC cockpit cabin power outlet
  • Cockpit panel sun-glare shields
  • Overhead cockpit windows sun shades
  • Floor provisions for 15-seat configuration
  • Fluorescent lighted emergency exit signs
  • Cockpit map and data case in central console
  • Two flash lights for pilot and co-pilot
  • Map and data cases in pilot and co-pilot doors
  • ICS panel with plug for one headset
  • Air ventilation system
  • First aid kit 


  • Two color polyurethane painting in accordance with SELLER’s standard painting scheme


  • Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery connector warning flag (1)
  • Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue
  • Tie-down assemblies for main rotor blades (5)
  • Tail rotor blades flapping block (1)
  • Main rotor blades sock pole (1) ,
  • Main landing gear wheel chocks (2)
  • Main rotor balance and tracking chart, tail rotor balance chart
  • Nose landing gear center pin (1) and landing gear handle locking pin (1 )
  • Jacking dome assy (1)
  • Tow bar (1)
  • Loose equipment bag (1)


  • SAGEM ICDS-10 MFD (Installed option)
  • 2 EFBs w/Jeppesen Charts (Installed option)
  • 2 Honeywell RT-300 Radar Altimeters


  • Air Conditioning
  • Super Slient MGB
  • Aux Fuel Tank Provision
  • Emergency Floats
  • 7 Cameras + 1 Infrared Camera
  • Mast Vibr Absorber w /3rd Vibration Absorber
  • Baggage Compartment Smoke Detector
  • Pilot & Co-pilot Smoke Detector
  • Heated Windshield
  • Pilot & Co-pilot Adjustable Seats
  • Pax Cabin Tinted Window
  • Pilot Sliding Storm Window
  • Nose Landing Gear Doors
  • Deluxe Metallic Color Paint Scheme
  • Heads-Up Checklist
  • Heads-Up Pax Briefing System
  • Pilot & Co-pilot Chart Holders
  • Pulse Lights Rosen
  • Sun Visor System
  • Hydraulic Pulsation Dampers
  • Dual Sliding Doors Electric
  • Electrically operated pax step ,(RH and LH) with boarding lights (in lieu of fixed steps)
  • Aux Heavy Duty Battery

EXTERIOR Light Metallic Sanstone with White Stripe and Brown Accents INTERIOR

  • Custom Pininfarina VIP Leather Interior Cocoon Generation II
  • Noise Reduction Interior
  • Two–Zone Climate Control
  • 9 Pax Interior consisting of the following:
    • 4 rear -facing seats seats
    • 2 VVIP forward-facing seats
    • 3 (removable)rear-facing middle jump seats
  • Custom Refreshment Cabinet & Entertainment
  • Electrically operated Limo Clear/Covered Panels between Cabin & Cocpit
  • Deluxe VIP Entertainment w/Two 15” Monitors w/Airshow Mapping DVD / CD/Satellite Radio / I-Pod Capability w/Touchscreen
  • 8 Speakers and Woofer Sound System w/ Outboard Seat Vol. Controls
  • Cabin Ceiling Natural Lighting on Front and Aft Cabin
  • Cabin Intercommunication System
  • SATCOM Iridium ST3100 AIR Air Cell ( ICS integrated with cabinset)


  • Maintained at Agusta Service Center since New
  • All Mandatory Ads & SBs, & Inspections per Manufacturer completed.