Agusta AW139 For Sale -2013

  This unit has under 900 hrs 

  Is the highest specification V-VIP machine on the market 

  Please contact us directly for price and specifications. 

AIRFRAME

• Aluminium alloy fuselage
• Acrylic 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 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 passenger 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 M/R 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)
•  Rotor brake
•  Provision for main rotor tracking (magnetic pick-up)

POWER PLANT AND FUEL SYSTEM

• Two Pratt & Whitney Canada PT6C-67C turboshafft engines
• Two independent FADEC systems with autostart and engine control functions for normal, emergency and training operations
• Two magnetic chip detectors
• Two integrated and independent engine oil coolers
• Separation 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

 

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 gauge 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 conditioning compressor quill

 

 

 

 

 

ELECTRICAL SYSTEMS

• 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)    
• Anticollision light
• External emergency landing lights on the sponsons (2)
• Fixed landlng/taxing lights on the sponsons (2)
• Retractable/rotating landing light
• Baggage compartment lights (3) and smoke sensor

 

STANDARD AVIONIC PACKAGE

• 1st PFD (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
• 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" * 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" * 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 (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) Basic
• Provision for CVR/FDR data interface (single)
• Flight Director System (dual)
  • Pilot and co-pilot 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/MB
  • Right Modular Radio Cabinet (MRC) with the following modules:
•           One VHF Comm.
•           One Mode S diversity transponder VOR/LOC/GS/MB
•           One ADF
•           One DME
  • Two pedestal mounted Multi Control Function Display Units (MCDU)
  • 1st radar altimeter RT-300
  • 2nd radar altimeter RT-300
  • Emergency Locator Transmitter (ELT)
  • 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 (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
• 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
• Air ventilation system
• First aid kit

ADDITIONAL EQUIPMENT

• Air Conditioning
• Customized painting scheme, metallic colours from Company selection
• Pilot/co-pilot adjustable seats (4G) in lieu of standard seats
• Sheep cover for pilot/co-pilot seats
• Co-pilot hinged window (storm window)
• Pilot and co-pilot glass windshield
• Pilot and co-pilot headsets Bose ANR (in lieu of standard headset),
• Pilot headset hooks (Qty 2)
• Approach plates chart holders with lights for pilot and co-pilot
• 4-axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hover Mode (HOV)
• Auxiliary heavy duty battery 27 Ah (in lieu of 13 Ah)
• Enhanced Ground Proximity Warning System (EGPWS) provision
•  Enhanced Ground Proximity Warning System (EGPWS) removable
• GPS 2nd unit (installation)
• 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 installation
• Camera on the tail fin
• Emergency floats provisions    
• Engine air particle separators provision
• Secondary swivelling landing light - in lieu of taxi/landing light on the sponsons (2)
• Auxiliary transversal fuel tanks 132 USgal provision
• Auxiliary transversal fuel tanks 132 USgal removable
• EVS (Enhanced Vision System) EVS-1500 Max Viz (dual field of view and image processing/*** ) Under Fuselage
• Maritime protection
• Increased gross weight 6,800 Kg

 

 

 

 

 

 

INTERIOR

FIVESTAR CABIN INTERIOR -7 SEATS

(CONVERSION KIT FOR 9 PASSENGERS)

•     3 armchairs leather covered forward-looking (with inertial reels and safety belt, sliding inflight direction, reclining backrest), with the middle armchair foldable     forward and the 2 lateral armchairs with foldable table

•     Comfortable seat leather covered (Qty 4) (with safety belts, storage       compartment under the seats and under-seat skirts)

•     3 seats removable leather covered armrests

•     2 lateral covered armrests cabinets with metal cup holder, ICS control and           multipurpose holder

•     Multipurpose Cubby with 3 sliding doors

•     Separation wall leather and leatherette covered with manual sliding window and roll up curtain on pilot side

•     Passenger cabin sliding doors with liners leather/leathered covered with PSU

•     Super Silent soundproofing

•     Electrically operated pax steps (RH and LH) (in lieu of Fixed passenger steps)

•     Nose landing gear doors

•     Customized VIP cabin finishing

•     Decoration trim

•     Passenger carpet (high thickness)

•     Environmental Control System (with control panel in passenger cabin -1      FEEL control panel on armrests)

•     P.A. (Passenger Address) system (including loudspeakers and safety belts l ights)

•     ICS in the cabin for all passengers

•     Passenger cabin thermo acoustic double layer tinted windows (colour to be selected)

•     Ripple dampers

•     Active Vibration Control System   (AVCS) complete installation

•     MGB Premium grade

•     Mast Vibration Absorber 

•     Cyclic and collective leather gators (same colour as cabin interior)

•     2 metal finished cabin vertical handles on doorposts

•     Alternate current power outlet (Qty 3)

•     Coat hooks (Qty 4)

•     One ICS phone in the cabin for communicating with pilots located inside the     rear left armrest cabinet

•     2 additional comfortable seats leather covered with safety belts