2020 Leonardo AW139 for sale,

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Agusta AW139 Exterior
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Agusta AW139 Cabin
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Agusta AW139 Seats
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Agusta AW139 Seat Detail
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Agusta AW139 Cockpit
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Agusta AW139 controls
Please call
Europe
Year
2020
S/N
TBD
Reg
-
TT
Test Flight Hours

Aircraft Description

Brand new helicopter. Has only flown test flights
HEMS/SAR configuration
Increased Gross Weight

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AIRFRAME / ENGINES / APU / WEIGHT / TOTAL LANDING

AIRFRAME

Manufacturing Year: 2020
Total Time: Test Flight Hours
Landings:Test Flight Cycles
Location: Europe

ENGINES

Make:Pratt & Whitney Canada
Model:PT6C-67C
Times :# 1: Test Flight Hours
# 2: Test Flight Hours
Cycles:# 1: Test Flight Cycles
# 2: Test Flight Cycles
  • AVIONICS & CONNECTIVITY
    Standard Avionics Package
    -1stPFD (Pilot Primary Flight Display) 8" ×10" (external) color Active MatrixLiquid 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) color Active MatrixLiquid Crystal Display as part of Honeywell Primus Epic System for visualization of flight and navigation data
    -1stMFD (Pilot Multi-Function Display) 8" ×10" (external) color Active MatrixLiquid 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) color Active MatrixLiquid 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)
    -Pilot and co-pilot headsets
    -Pilot and co-pilot interphone control (cyclic grip and floor switches)
    -Pilot clock (digital)
    -Co-pilot clock (digital)
    -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)
    -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 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
    -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
    -1stradar altimeter RT-300
    -2ndradar 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 color from Company selection
    -Main rotor blades high visibility painting
    -Cockpit tinted upper window (*)Smoked color
    -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
    -4-axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hover Mode (HOV)
    -Auxiliary transversal fuel tanks 132 US gal provision
    -Auxiliary transversal fuel tanks 132 US gal Removable
    -Engine wash kit
    -HF radio

    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)

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