2013 AW139
NOT ADVERTISED ON THE GENERAL MARKET

Only approx. 972 hrs TT
Five Star Cabin Interior (7 seats) with Removable Centre Table/Cabinet & Conversion Kit for 9 pax
Environmental Control System (with control panel in passenger cabin -1 FEEL control panel on armrests)
Super Silent soundproofing & Passenger Address system

INTERIOR LAYOUT

3 leather covered armchairs fwd-looking (with inertial reels and safety belt, sliding inflight direction, reclining backrest),
Middle armchair foldable fwd & the 2 lateral armchairs with foldable table
Comfortable seat leather covered (Qty 4) (with safety belts, storage compartment under the seats and under-seat skirts)
3 seats removable leather covered armrests
2 lateral covered armrests cabinets with metal cup holder,
Centre Table / Storage Cabinet (Removable)
Passenger cabin sliding doors with liners leather/leathered covered with PSU
Customized VIP cabin finishing with luxurious carpet depth
Environmental Control System (with control panel in passenger cabin -1 FEEL control panel on armrests)
P.A. system (including loudspeakers and safety belts lights)
Super Silent soundproofing
ICS in the cabin for all passengers – ICS control and multipurpose holder
Passenger cabin thermo acoustic double layer tinted windows

AVIONIC PACKAGE INCLUDES:

Honeywell GPS module with Flight Plan Management System (FPMS)
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)
cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
1st PFD (Pilot Primary Flight Display 8″ x 10″ 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″ x 10″ colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
1st MFD (Pilot Multifunction Display 8″ * 10″ colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data
2nd MFD (Co-pilot Multifunction Display 8″ * 10″ 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
4-axis dual Digital Automatic Flight Control System (DAFCS) Basic
Provision for CVR/FDR data interface (single)
Flight Director System (dual)
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 Mode S diversity transponder -One VOR/LOC/GS/MB
One ADF, One DME
Two pedestal mounted Multi Control Function Display Units (MCDU)
1st radar altimeter RT-300 – 2nd radar altimeter RT-300
Emergency Locator Transmitter (ELT)
One flight guidance controller

OTHER FEATURES

Electrically operated pax steps (RH and LH) (in lieu of Fixed Steps)
Nose landing gear doors
Ripple dampers
Active Vibration Control System (AVCS) complete installation
MGB Premium grade
Mast Vibration Absorber
Cyclic and collective leather gators (same colour as cabin interior)
2 metal finished cabin vertical handles on doorposts
Alternate current power outlet (Qty 3)
ICS phone in the cabin for communicating with pilots located inside the rear left armrest cabinet
2 additional comfortable seats leather covered with safety belts

ADDITIONAL EQUIPMENT & FEATURES

Customized metallic paint scheme
Pilot/co-pilot adjustable seats (4G) in lieu of standard seats
Sheep cover for pilot/co-pilot seats
Co-pilot hinged window (storm window)
Pilot and co-pilot glass windshield
Pilot and co-pilot headsets Bose ANR (in lieu of standard headset),
Approach plates chart holders with lights for pilot and co-pilot
4-axis DAFCS (Digital Automatic Flight Control System)
Enhanced with Hover Mode (HOV)
Auxiliary heavy duty battery 27 Ah (in lieu of 13 Ah)
Enhanced Ground Proximity Warning System (EGPWS) provision
Enhanced Ground Proximity Warning System (EGPWS) removable
GPS 2nd unit (installation)
TCAS I KTA-970 Honeywell Bendix/King provision
TCAS I KTA-970 Honeywell Bendix/King removable
Weather Radar Primus 660 Honeywell provision
Weather Radar Primus 660 Honeywell installation
Camera on the tail fin
Secondary swivelling landing light – in lieu of taxi/landing light on the sponsors (2)
Auxiliary transversal fuel tanks 132 US gal provision
Auxiliary transversal fuel tanks 132 USgal removable
Maritime protection
Increased gross weight 6,800 Kg