2018 Leonardo AW139 For Sale, China

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Leonardo AW139 1
Please call
Asia, China
Year
2018
S/N
-
Reg
-
TT
Delivery hours only

Aircraft Highlights

For Immediate Sale

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Asian Sky Group
  • AIRFRAME / ENGINES / APU / WEIGHT / TOTAL TIME / TOTAL LANDING

    AIRFRAME

    Delivery Hours & Cycles Only

    ENGINES

    Two Pratt & Whitney Canada PT6C-67C turbo-shaft engines
    Two independent FADEC systems with auto-start and engine control functions for normal, emergency and training operations
    Two magnetic chip detectors
    Two integrated and independent engine oil coolers
    Separation firewall protection for each engine
    Fire detection system
    Fire extinguisher system (2 bottles)
    Steel engine exhausts and ejectors
    Two independent crashworthy fuel cells
    Two supply pumps on engines
    Two submerged booster pumps in fuel tank
    Two fuel filter assemblies
    Two engine back-up controls, mechanical and electrical
    Two manual engine start and ignition systems

    TOTAL TIME

    Delivery hours only
  • AVIONICS & CONNECTIVITY
    1st PFD (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
    2nd PFD (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
    2nd MFD (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
    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)

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