2013 AGUSTA AW139 For sale

2007 Agusta Westland 139 For Sale

2013 Agusta AW139 For Sale - Serial Number 31466

Serial Number 31466  |  TC-HVK
Aircraft Offered Subject to Prior Sale or Withdrawal from Market. Specifications Subject to Verification by Buyer.

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OVERVIEW

Year of Manufacture: 2013
Air Frame Total Time: 826 Hours
Total Landings Since New: 2,210

•Engines on ESP Gold Lite
•Avionics on Honeywell HAPP
•Camera on Tail Fin
•EVS-1500 MaxViz Enhanced Vision System
•Primus Epic Phase 7
•Auxiliary Transversal Fuel Tanks 132 Gallon
•EGPWS
•Emergency Floats with Kevlar Covers
•4 Axis DAFCS Enhanced with Hover Mode

ENGINES
Pratt & Whitney PT6C-67C
Engine 1: 826 Hours | Cycles 1,083
Engine 2: 826 Hours | Cycles 1,083
 

ADDITIONAL OPTIONS

•Customized painting scheme, metallic colors from Company selection
•Pilot/co-pilot adjustable seats (4G) in lieu of standard seats
•Sheep skin cover for pilot and co-pilot seats
•Pilot and co-pilot Glass windshield
•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/removable
•TCAS I KTA-970 Honeywell Bendix/King provision/removable
•Weather Radar Primus 660 Honeywell provision/installation
•Emergency floats provision/removable
•Emergency floats Kevlar covers
•Auxiliary transversal fuel tanks 132 USgal provision/removable
•Increased gross weight - 6.800 kg
•Co-pilot hinged window (storm window)
•Pilot and co-pilot headsets Bose ANR type (in lieu of standard headsets)
•Pilot headset hooks (Qty 2)
•GPS 2nd unit
•EVS-1500 MaxViz (dual field of view and image processing)
•Maritime Protection
•Engine air particle separators provision
•Camera on the tail fin
•Primus Epic Phase 7
•Electrically operated pax steps LH / RH 

INTERIOR

FIVESTAR Cabin Interior (7 seats), including:

•3 armchairs leather covered-forward looking, middle one can be folded forward (with inertial reels and safety belt, sliding inflight direction, reclining backrest)
•1 Divan seat leather covered (with 4 safety belts and understorage compartment)
•1 leather covered armrest installed in the middle of Divan seat)
•2 lateral covered armrests cabinets with metal cupholder, ICS control and multipurpose holder installed on the divan seat)
•2 lateral covered armrests cabinets with metal cupholder, ICS control and multipurpose holder installed on 3 armchairs)
•Multipurpose Cubby with 3 sliding doors
•Night curtain cabin separator
•Passenger cabin sliding doors with liners leather/leathered covered with PSU
•Super Silent soundproofing
•Nose landing gear doors
•Customized VIP cabin finishing
•Decoration trim
•Standard passenger carpet in lieu of High thickness passenger carpet
•Environmental Control System (with control panel in passenger cabin - IFEEL control panel on armrests)
•P.A. (Passenger Address) system (including loudspeakers and safety belts lights)
•ICS in the cabin for all passengers including two additional seats in the middle
•Passenger cabin thermo acoustic double layer tinted windows
•Ripple dampers
•AVCS complete installation
•MGB Premium grade
•MVA
•Cyclic and collective leather gators (same color as cabin interior)
•2 metal finished cabin vertical handles on doorposts
•Alternate current power outlet (Qty 3)
•Coat hooks (Qty 4)
•One ICS phone located inside the rear left armrest cabinet in the cabin for communicating with pilots
•2 additional comfortable seats leather covered with safety belts

 

INTERIOR EQUIPMENT

•Pilot and co-pilot crashworthy seats (w/ inertial reels & safety belts)
•Cockpit dome/storm light
•Cockpit utility lights (2)
•28 V 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 co-pilot
•Map and data cases in pilot and co-pilot doors
•ICS panel with plug for one headset
•Air ventilation system
•First aid kit
 

MISCELLANEOUS/GROUND EQUIPMENT

•Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery connector warning flag (1)
•Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue
•Tie-down assemblies for main rotor blades (5)
•Tail rotor blades flapping block (1)
•Main rotor blades sock pole (1)
•Main landing gear wheel chocks (2)
•Main rotor balance and tracking chart, tail rotor balance chart
•Nose landing gear centre pin (1) and landing gear handle locking pin (1)
•Jacking dome assy (1)
•Tow bar (1)
•Loose equipment bag (1)

AVIONICS

STANDARD AVIONIC PACKAGE

•1st PFD (Pilot Primary Flight Display 8" × 10" color Active Matrix LCD) as part of Honeywell Primus Epic System for visualization of flight and navigation data
•2nd PFD (Co-pilot Primary Flight Display 8" × 10" color Active Matrix LCD) as part of Honeywell Primus Epic System for visualization of flight and navigation data
•1st MFD (Pilot Multifunction Display 8" × 10" color Active Matrix LCD) as part of Honeywell Primus Epic System for visualization of flight and navigation data
•2nd MFD (Co-pilot Multifunction Display 8" × 10" color Active Matrix LCD) 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
 

For more information on this aircraft, please contact us using the form below, by email AW139@AltusAviation.com or by phone in the EU +4917662555634 or the US +1 888 337 3439.

 

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For More Information: US: +1-888-337-3439 | EU: +49 1766 255 5634 | info@altusaviation.com