• London: +44(0)1959 576 017
  • Agusta AW139: 2011

    Agusta AW139: 2011

    MODEL Agusta AW139
    YEAR OF MANUFACTURE 2011
    AIRFRAME HOURS 868 hrs
    PRICE POA

    Features:

    Full Anti Ice System – FIPS

    6800 kgs Increased Weight Option.

    4 Year Inspection Complete

    Engines:  2 x Pratt & Whitney Canada PT6C-67C

    Exterior: White metallic paintwork with dark blue accent paintwork around windows

    VIP Six Seat Cabin Layout Interior: 

    • 2 Captain seats leather covered (with inertial reels sliding inflight direction, reclining backrest and separate 4 points safety belts)
    • Bench seat consisting of 4 leather covered individual seats and arm rests (with safety belts and under- seat skirts)
    • Headsets Bose ANR type
    • Fashion cabinet with refrigerated drawer
    • Roundy cabinet, with dual direction TV screen, and drinks storage
    • 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) with boarding lights (in lieu of fixed steps)
    • Nose landing gear doors
    • Customized VIP cabin finishing
    • Passenger carpet (high thickness)
    • Air conditioning system
    • P.A. (Passenger Address) system (including loudspeakers and safety belts lights)
    • ICS (ifeel entertainment system) in the cabin for all passengers
    • Passenger cabin therm acoustic tinted double layer windows
    • Hydraulic pulsation dampeners
    • Active Vibration Control System (AVCS) complete installation
    • 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/115V 50 Hz) (Qty 4)
    • Coat hooks (Qty 4)
    • Passenger cabin hinged doors
    • Pilot and co-pilot adjustable leather covered seats.
    • Pilot headset hooks (Qty 2)
    • 7th seat (captains seat) in lieu of fashion cabinet

    Avionics:

    • 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″ 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

    Equipment:

    • Central Maintenance Computer – CMC (single)
    • Two VHF Comm
    • One Mode-S Diversity Transponder
    • One VORILOC/GSIMB – One ADF One DME
    • Two pedestal mounted MCDUs (Multi Control Function Display Units)
    • Pilot and co-pilot interphone control (cyclic grip and floor switches)
    • 1st Radar Altimeter (RT – 300) 2nd Radar Altimeter System (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)
    • Magnetic compass Outside
    • Air Temperature indicator
    • Two (2) Master Warning Lights (MWLs)
    • Two (2) Master Caution Lights (MCLs)
    • Engine 1 Fire Light — Engine 2 Fire Light
    • Two (2) Master Warning Lights (MWLs), Two (2) Master Caution Lights (MCLs)
    • 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)
    • One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data)
    • Two (2) Attitude and Heading Reference Systems (AHRSs)
    • Two (2) Air Data Modules (ADMs)
    • Two (2) flux valves Two (2) Display Controllers (DCs)
    • Two (2) Cursor Control Devices (CCDs)
    • Reversion Control Panel (RCP)
    • Display Dimming Control Panel (DCP)
    • Stability Augmentation System (SAS) control panel
    • Two (2) Remote Instrument Controllers (RICs)
    • 4-Axis Digital Automatic Flight Control System – DAFCS (dual) with auto trim function CVR/FDR
    • Flight Director System (dual) , Pilot and co-pilot microphone and headset
    • Two Modular Avionic Units (MAUs
    • Monitor Warning System – MWS (dual) Aural Walling Generator – AWG (single)

    Additional Equipment

    • IFR Configured
    • Auxiliary fuel tank provision
    • Air conditioning
    • Emergency floats
    • Additional anti-collision light under fuselage
    • TCAS I Bendix King fixed provisions
    • TCAS I Bendix King KTA-970
    • Weather radar (Primus 660) fixed provisions
    • Baggage Load Capacity Increase to 300 kg
    • Central Approach Plates Chart Holders with Light
    • Strobe Light on the Sponson/Elevator
    • VHF/FM NPX-138 NAT Tactical Radio
    • Aircell Satphone.