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  • Alert Me Name: Leonardo AW139
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Leonardo AW139
Please Call
  • YEAR
    2019
  • LOCATION
    Asia, China
  • S/N
  • REG
  • TTAF
    Delivery hours only

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
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)

Leonardo AW139

Please Call
  • YEAR
    2019
  • LOCATION
    Asia, China
  • S/N
  • REG
  • TTAF
    Delivery hours only
User Image
Jeffrey C. Lowe
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