2009 LEONARDO AW139


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    Aircraft Summary


    General

    Year
    2009
    Manufacturer
    LEONARDO
    Model
    AW139
    Serial Number
    X
    Condition
    Used
    Description
    • One Corporate Owner Since New • 12 Seats Corporate / Passenger Configuration with Soundproofing • Always Hangared • Air Conditioning System • Emergency Floating System • HUMS, Weather Radar, EGPWS, TCAS • Heated Windshield • Active Vibration Control System

    Airframe

    Total Time
    3326
    Airframe Notes
    MANUFACTURING YEAR: 2009 SERIAL NUMBER: 31260 TOTAL HOURS: 3,326 Since New TOTAL CYCLES: 6,909 Since New

    Engine 1

    Engine 1 Notes
    MODEL: P&W Canada PT6C–67C SERIAL NUMBER: PCE-KB0569 TOTAL HOURS: 3,326 Since New OTHER FEATURES: FADEC Systems (One on Each Engine)

    Engine 2

    Engine 2 Notes
    MODEL: P&W Canada PT6C–67C SERIAL NUMBER: PCE-KB0540 TOTAL HOURS: 3,326 Since New OTHER FEATURES: FADEC Systems (One on Each Engine)

    Avionics

    Avionics/Radios
    • Dual PFD (8” × 10” Pilot Primary Flight Display) • Dual MFD (8” × 10” Pilot Multifunction Display) • One Electronic Standby Instrument System (ESIS) • 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 (RICs) • 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 - AWG (single) - Central Maintenance Computer - CMC (single) - 3–Axis Digital Automatic Flight Control System - DAFCS (dual) with autotrim function • Provision for CVR/FDR data interface (single) • Flight Director System (dual) • Pilot and Copilot microphone and headset • Pilot and Copilot 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 VOR/LOC/GS/MB - One ADF - One DME • Two pedestal mounted MCDUs (Multi Control Function Display Units) • 1st Radar Altimeter (RT – 300) • 2nd Radar Altimeter System (RT – 300) • Emergency Locator Transmitter (ELT –121.5/243/406 MHz) • One Flight Guidance Controller • Honeywell GPS module with Flight Plan Management System (FPMS) • Pilot and copilot digital audio panels with remote ICS audio port for ground operation • Pilot clock (digital) • Copilot clock (digital) • One magnetic compass • One Outside Air Temperature indicator • Two Master Warning Lights (MWLs) • Two 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)

    Additional Equipment

    Additional Equipment
    • Limited 4-Axis DAFCS • Enhanced Ground Proximity Warning System (EGPWS) • Ice Detector • HUMS • Emergency Floating System (provision and removable parts) • Kevlar rigid covers for Emergency Floats • Pilot and co-pilot adjustable seats • Heated Windshield • Active Vibration Control System (AVCS)

    Exterior

    Exterior Notes
    Customized painting scheme in metallic color with extra coating: Two color polyurethane painting in accordance with OEM standard painting scheme

    Interior

    Interior Notes
    CORPORATE cabin basic arrangement: • Silent soundproofing • Standard roof liners with LED dome lights • Composite liners leatherette covered • Passenger carpet • ICS panel, one position in passengers cabin (LH side) • P.A. (Passenger Address) System (including loudspeakers and safety belts lights) • Fixed steps for passenger cabin access CORPORATE 12 seats interior configuration: • 12-padded crashworthy comfortable seats fabric or leatherette covered (with inertial reels and safety belts) disposed on 3 rows • Air conditioning Additional Proposed Equipment: • MGB Premium grade • Mast Vibration absorber (MVA) • Passenger cabin thermo acoustic double layer tinted windows • Ripple dampers Standard Item / Equipment: • Cabin, cockpit and baggage compartment utility finishing interior • Pilot/ Copilot 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 • Floor provisions for 15-seat configuration • Fluorescent lighted emergency exit signs • Cockpit map and data case in central console • Two flash lights for pilot and copilot • Map and data cases in pilot and copilot doors • ICS panel with plug for one headset • First aid kit • Air ventilator system


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