2018 Leonardo AW139 For Sale, China

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Leonardo AW139 Exterior
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Leonardo AW139 interior cabin
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Leonardo AW139 Interior
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Leonardo AW139 Seating
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Leonardo AW139 Seating View
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Leonardo AW139 interior stretcher
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Leonardo AW139 Panel
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Leonardo AW139 Exterior take off
Please call
Asia, China
Year
2018
S/N
41542
Reg
B-704S
TT
238

Aircraft Description

HEMS/SAR Configuration
Increased Gross Weight
Low hours
Well maintained

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Jet 8
  • AIRFRAME / ENGINES / APU / WEIGHT / TOTAL TIME / TOTAL LANDING

    AIRFRAME

    Total Time: 238 Hours (As of June 2020)
    Landings:328

    ENGINES

    Manufacturer:Pratt & Whitney Canada
    Model: PT6C-67C
    #1#2
    Serial Number: PCE-KB2120PCE-KB2118
    Total Time:238 Hours 320 Hours
    Cycles:214214

    TOTAL TIME

    238
  • Maintenance & Inspections
    Next 1Yr Inspection Due on 12th September 2020
  • AVIONICS & CONNECTIVITY
    Standard Avionics Package
    1stPFD (Pilot Primary Flight Display) 8" ×10" (external) colourActive Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    2ndPFD (Co-pilot Primary Flight Display) 8" ×10" (external) colourActive Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    1stMFD (Pilot Multi-Function Display) 8" ×10" (external) colourActive Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    2ndMFD (Co-pilot Multi-Function Display) 8" ×10" (external) 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
    Provision for CVR/FDR data interface (single)
    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
    1stPFD (Pilot Primary Flight Display) 8" ×10" (external) colour Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    2ndPFD (Co-pilot Primary Flight Display) 8" ×10" (external) colour Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    1st MFD (Pilot Multi-Function Display) 8" ×10" (external) colour Active Matrix Liquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    Right Modular Radio Cabinet (MRC) with the following modules:
    One VHF Comm.
    One VOR/LOC/GS/MB
    One ADF
    One DME
    Two pedestal mounted Multifunction Control Display Units (MCDU)
    Emergency Locator Transmitter (ELT)
    One flight guidance controller
    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)
  • Additional Equipment & Information
    AW139 Standard Equipment
    Forced fan ventilation
    Bleed air heater and defroster with air noise suppressions
    Cockpit air ventilation system
    Baggage compartment cargo tie-down fittings for increased load capacity (up to 300 kg)
    Rotor brake
    1st radar altimeter RT-300
    2nd radar altimeter RT-300
    4-axis dual Digital Automatic Flight Control System (DAFCS) Basic incorporated into Modular Avionic Units (MAUs)
    Flight Director System (dual) incorporated into the Modular Avionic Unit (MAU)
    Two Honeywell GPS modules (GNSS/SBAS –Global Navigation Satellite System/Satellite Based Augmentation System) with Flight Plan Management System (FPMS)
    One Mode S diversity transponder with Extended Squitter (ADSB-Out 1090 MHz) incorporated into the Modular Radio Cabinet (MRC)
    Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
    Health & Usage Monitoring System (HUMS)
    Increased Payload Package -Increased Gross Weight -6,800 kg

    Additional Optional Equipment
    AgustaWestland painting scheme, metallic colour from Company selection
    Main rotor blades high visibility painting
    Cockpit tinted upper window (*)Smoked colour
    Co-pilot hinged window (storm window)
    Approach plates chart holders with lights for pilot and co-pilot
    (*) Required for single pilot IFR operations. Alternative to central approach plate chart holder
    Air conditioning system
    (*) Accessory drive is required if the air conditioning system is installed in conjunction with FIPS
    Weather Radar Primus 660 Honeywell -Provision
    Weather Radar Primus 660 Honeywell -Removable
    Cargo hook (2200 kg / 4850 lb) -Provision
    (*) Including cargo hook monitoring cameras provision
    Emergency floats -Provision
    Rescue hoist (Breeze) -provision
    (*) Including: ICS AV-900 Honeywell and Wireless ICS Polycon
    Rescue hoist (Breeze) -Removable
    (*) Including light
    Strobe lights on the winglets
    Bubble cabin window (LH and RH)
    (*) Not compatible with passenger cabin vertical sliding windows on fixed windows
    -Increased gross weight 7,000 Kg
    Power outlet 110V
    Cabin Door Lighting
    Ice Detector (RAD)
    Standard roof liners with dome lights
    Composite liners –painted(no soundproofing)
    Rail Floor
    Qty 3 Foldable passenger seats –3rd row
    Qty 1 lightweight crashworthy passenger seat –1st row
    -axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hover Mode (HOV)
    Auxiliary transversal fuel tanks 132 USgalprovision
    Auxiliary transversal fuel tanks 132 USgalRemovable
    Engine wash kit
    HF

    Miscellaneous / Ground Equipment
    Cargo net in baggage compartment for increased load capacity (up to 300 kg)
    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 centrepin (1) and landing gear handle locking pin (1)
    Jacking dome assy(1)
    Tow bar (1)
    Loose equipment bag (1)

    WiFi

    No

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