2009 Leonardo AW139 for Sale

Only 2 Corporate Owners Since New 12 Seats Corporate / Passenger Configuration with Soundproofing Always Hangered Air Conditioning System Emergency Floatation System HUMS, Weather Radar, EGPWS, TCAS Heated Windshield Active Vibration Control System AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT AIRFRAME Entry into Service: 2009 Total Time: 3,434 Hours Total Cycles: 7,113ENGINES Make: Pratt & Whitney Model: PT6C-67C TSN: 3,434 hours TSO: 7,113 hours AVIONICS & CONNECTIVITY • 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 & Information CORPORATE 12 seats interior configuration: 12-padded crashworthy comfortable seats fabric or leatherette covered (with inertial reels and safety belts) disposed on 3 rows CORPORATE cabin basic arrangement: • Air conditioning • 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 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 • Limited 4-Axis DAFCS • Moving map Sky Force Observer MKIII with std aeronautics charts • Honeywell Primus 660 Weather radar • Ice Detector • Storm Window for the Copilot • HUMS • Additional Anti-Collision Light • Strobe Lights • Emergency Floating System (provision and removable parts) • Kevlar rigid covers for Emergency Floats • Pilot and co-pilot adjustable seats (in lieu of std seats) • Customized leather covering for Pilot and co pilot seats (same color as interior) • Heated Windshield • Enhanced Ground Proximity Warning System (EGPWS) (provision and removable parts) • TCAS I KTA-970 Honeywell Bendix/King (provision and removable parts) • Approaches Plates chart holder with light for pilot and co-pilot • Auxiliary Heavy Duty battery 27 Ah (in lieu of 13 Ah) • Active Vibration Control System (AVCS) provision • Active Vibration Control System (AVCS) installation