2013 AgustaWestland - AW139 SN60001
Aircraft
  • Manufacturing Year: 2013
  • Serial Number: 60001
  • Total Hours: 384 Since New
  • Asking Price: Make Offer
Aircraft Highlights
  • 2+6 Leather Seats VIP Configuration w/ Conversion Kit for 8 Passengers
  • Incrased Gross Weight - 6,800 KG
  • Air Conditioning System
  • Super Silent Soundproofing
  • Emergency Floats (Fixed Parts)
  • Wire Strike Protection System
  • Passenger Cabin Hinged Doors
  • Anti-icing System
Engines
Engines Model: PW Canada PT6C-67C Turboshaft
  • Total Hours: 384 Since New
Aircraft Basics
  • Aluminum alloy fuselage
  • Acrylic windshields
  • Overhead cockpit transparent windows
  • Lower cockpit transparent windows
  • Cockpit ram air adjustable outlets
  • Forced fan ventilation
  • Bleed air heater and defroster with air noise suppressions
  • Heated Pitot tubes (2) with Pitot heat failure warning (2)
  • Heated static intakes (2)
  • One cockpit and one passenger cabin fire extinguisher
  • Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side)
  • Plug-in sliding doors (2) for passengers cabin access with four locking latches
  • Passenger doors stop in fully open position
  • Six cabin push-out emergency exit windows (two on each passenger cabin door)
  • Baggage compartment with two 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
Rotors and Controls
  • Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers
  • Rotating MIR flight controls
  • Main rotor hub beanie
  • 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)
Power Plant & Fuel System
  • Two Pratt & Whitney Canada PT6C-67C turboshaft engines
  • Two independent F ADEC systems with auto start and engine control functions for normal, emergency and training operations
  • 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 submerged in fuel tank
  • Two fuel filter assemblies
  • Two engine back-up controls, mechanical and electrical
  • Two manual engine start and ignition systems
Transmission Drive System and Hydraulic System
  • 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 (PCMs)
  • 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 conditioning compressor quill
Electrical System
  • 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 44 Ah main battery plus one 13 Ah auxiliary battery
  • DC Starter Generator Control Units (2)
  • Navigation lights (3)
  • Anti-collision light
  • External emergency landing lights on the sponsons (2)
  • Fixed landing/taxi lights on the sponsons (2)
  • Retractable/rotating landing light
  • Baggage compartment lights (3) and smoke sensor
Avionics
Standard Avionics Package
  • 1st PFD (Pilot Primary Flight Display 8” x I0” colour 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” colour 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” colour 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” colour 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 (AHRSs)
  • Two Air Data Modules (ADMs)
  • Two flux valves
  • Two Display Controllers (DCs)
  • Two Cursor Control Devices (CCDs)
  • One Reversion Control Panel (RCP)
  • One Display Dimming Control Panel (DCP)
  • One Stability Augmentation System (SAS) control panel
  • Two Remote Instrument Controllers (RlCs)
  • Two Modular Avionic Units (MAUs) incorporating the following major subsystems and/or functions:
  • Vehicle Monitoring System - VMS (dual)
  • Monitor Warning System - MWS (dual)
  • Aural Warning Generator - A WG (single)
  • Central Maintenance Computer - CMC (single)
  • 4-Axis Digital Automatic Flight Control System - DAFCS Basic
  • Provision for CVR/FDR data interface (single)
  • Flight Director System (dual)
  • Pilot and co-pilot headsets
  • Pilot and co-pilot interphone control - (cyclic grip and floor switches)
  • Left Modular Radio Cabinet (MRC) with the following modules:
  • One VHF Comm
  • One VOR/LOC/GS/MB
  • Right Modular Radio Cabinet (MRC) with the following modules:
  • One VHF Comm
  • One Mode-S diversity transponder
  • One YOR/LOC/GS/MB
  • One ADF
  • One DME
  • Two pedestal mounted MCDU (Multi - Control Function Display Units)
  • 1st Radar Altimeter (RT-300)
  • 2nd Radar Altimeter System (RT-300) Emergency Locator Transmitter
  • 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 operation
  • Pilot clock (digital)
  • Co-pilot 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 requirement compliant)
  • Cockpit Voice Recorder & Flight Data Recorder (CYR/FDR) with Underwater Locator Beacon (ULB)
Additional Installed Equipment
  • Passenger cabin hinged doors (RH and LH)
  • “Roundy” Cabinet + Entertainment package (including CD/DVD player; 2 display 17” LCD) + Jet map
  • Customized painting scheme
  • Main rotor blades high visibility painting
  • Approach plates chart holders with lights for pilot and co-pilot
  • Windshield washing system
  • 5th display in cockpit (stand-alone)
  • ADF 2nd unit (Fully installed)
  • Auxiliary heavy duty battery 27 Ah (in lieu of 13 Ah)
  • Enhanced Ground Proximity Warning System (EGPWS) (provision & removable)
  • GPS, 2nd (provision and removable)
  • HF/SSB Transceiver Primus HF- I 050 Honeywell provision
  • Moving Map EuroNav V with standard aeronautical charts provision
  • Moving Map EuroNav V (stand-alone) with standard aeronautical charts (removable)
  • TCAS I KTA-970 Honeywell Bendix/King Provision
  • TCAS I KTA-970 Honeywell Bendix/King removable
  • Weather Radar Primus 660 Honeywell provision
  • Weather Radar Primus 660 Honeywell removable
  • Additional anti-collision light under fuselage
  • Anti-icing system/combined accessory gear box
  • Auxiliary transversal fuel tanks 132 USG provision
  • Auxiliary transversal fuel tanks 132 USG removable
  • Emergency floats provision
  • Increased gross weight - 6.800 kg
  • Life rafts (Qty 2) up to 17 passengers each provision
  • Snow skids/slump protection pads provision
  • Anti sinking pads removable (tow bar adapter included)
  • Wire strike protection system
  • SATCOM Aircell 3100
  • Russian certification kit
Miscellaneous / Ground Equipment
  • 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 mam rotor blades (5)
  • Tail rotor: blades flapping block (1)
  • Main rotor blade sock pole (1)
  • Main landing gear wheel chocks (2)
  • Main rotor balance and tracking chart, tail rotor balance chart
  • Nose landing gear centre pin (1) and -landing gear handle locking pin (1)
  • Jacking dome assy (1)
  • Tow bar (1)
  • Loose equipment bag (1)
Interior & Cabin Equipment
  • 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 sunshades
  • Fluorescent lighted emergency exit signs
  • Cockpit map and data case in central console
  • Two flashlights 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
Five Stars Cabin Basic Arrangement, Including
  • Conversion kit for 8 passengers
  • 2 armchairs leather covered (with inertial reels sliding inflight direction, reclining backrest and separate 4 points safety belts)
  • Comfortable seat leather covered (with safety belts and under- seat skirts) (Qty 4)
  • Armrests leather covered for comfortable seats fwd. (Qty 3)
  • Lateral armrest-cabinets leather covered with metal cup holder (Qty 2)
  • Headsets Bose ANR type (Qty 6)
  • Fashion cabinet with newspaper holder and air conditioning control panel
  • Multipurpose Cubby with 3 sliding doors
  • Separation wall leather and leatherette covered with manual sliding window and roll up curtain on pilots side
  • Super Silent soundproofing
  • Electrically operated pax steps (RH and LH)
  • Nose landing gear doors • Customized VIP cabin finishing
  • Decoration trim
  • Passenger carpet (high thickness)
  • Air conditioning system
  • P.A. (Passenger Address) system (including loudspeakers and safety belts lights)
  • JCS in the cabin for all passengers
  • Passenger cabin thermo acoustic tinted double layer windows
  • Hydraulic pulsation dampeners
  • Active Vibration Control System Provision & Removable (AVCS)
  • MGB Premium Grade
  • Cyclic and collective leather gators (same colour as cabin interior)
  • Cabin vertical handles metal finished on doorposts (Qty 2)
  • Alternate Current (AC) power outlet (28V)
  • Coat Hooks (Qty. 4)
Printing
  • Standard colour scheme from HeliVert paint selection, solid colour
Specifications are subject to verification by purchaser upon Inspection. Aircraft is subject to prior sale and/or removal from the market without prior notice.