2013 AGUSTAWESTLAND - AW139 SN60001 for Sale

Description

Aircraft

Manufacturing Year: 2013
Serial Number: 60001
Total Hours: 384 Since New
Asking Price: Make Offer

Aircraft Highlights

2+6 Leather Seats VIP Configuration w/ Conversion Kit for 8 Passengers
Incrased Gross Weight - 6,800 KG
Air Conditioning System
Super Silent Soundproofing
Emergency Floats (Fixed Parts)
Wire Strike Protection System
Passenger Cabin Hinged Doors
Anti-icing System

Engines

Engines Model: PW Canada PT6C-67C Turboshaft

Total Hours: 384 Since New

Aircraft Basics

Aluminum alloy fuselage
Acrylic windshields
Overhead cockpit transparent windows
Lower cockpit transparent windows
Cockpit ram air adjustable outlets
Forced fan ventilation
Bleed air heater and defroster with air noise suppressions
Heated Pitot tubes (2) with Pitot heat failure warning (2)
Heated static intakes (2)
One cockpit and one passenger cabin fire extinguisher
Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side)
Plug-in sliding doors (2) for passengers cabin access with four locking latches
Passenger doors stop in fully open position
Six cabin push-out emergency exit windows (two on each passenger cabin door)
Baggage compartment with two lockable baggage compartment doors (LH and RH).
Baggage compartment cargo tie-down fittings
Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear)
Structural provisions for nose landing gear doors
Landing gear mooring
Upper deck mooring provisions
Hoisting and jacking fittings
Tail boom and vertical fin
Stabilizers with composite “winglets”
Pilot and co-pilot windshield wipers
Maintenance steps for access to upper deck on both sides
Upper deck cowlings (one front forward sliding, two side opening for engine access)
Steps for cockpit access
Anti-vibration masses (2) under cabin floor

Rotors and Controls

Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers
Rotating MIR flight controls
Main rotor hub beanie
Main dual servo actuators (3)
Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers
Rotating T/R flight controls One T/R dual servo actuator
Force trim system
Pilot fixed flight controls (cyclic, -collective, anti-torque pedals)
Co-pilot fixed flight controls (cyclic, -collective, anti-torque pedals)
Dual digital 3-axis linear actuators
Rotor brake
Provision for main rotor tracking (magnetic pick-up)

Power Plant & Fuel System

Two Pratt & Whitney Canada PT6C-67C turboshaft engines
Two independent F ADEC 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
Separate 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 submerged in fuel tank
Two fuel filter assemblies
Two engine back-up controls, mechanical and electrical
Two manual engine start and ignition systems

Transmission Drive System and Hydraulic System

Main transmission with two direct drive engine inputs
Three main transmission chip detectors/ debris collectors with burning capability
Two freewheel units
Four strut rods for upper deck attachment and one anti-torque plate
Intermediate gearbox with sight gauge and magnetic drain plug/chip detector
Tail gearbox with sight gage and magnetic drain plug/chip detector
Dual independent, redundant hydraulic systems
Two hydraulic Power Control Modules (PCMs)
Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation
One electrical pump for control checks on ground (engines off)
Air conditioning compressor quill

Electrical System

DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators
DC External Power Receptacle
Two Nickel-Cadmium Batteries: one 44 Ah main battery plus one 13 Ah auxiliary battery
DC Starter Generator Control Units (2)
Navigation lights (3)
Anti-collision light
External emergency landing lights on the sponsons (2)
Fixed landing/taxi lights on the sponsons (2)
Retractable/rotating landing light
Baggage compartment lights (3) and smoke sensor

Avionics

Standard Avionics Package

1st PFD (Pilot Primary Flight Display 8” x I0” 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” - x 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” x 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 (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 (RlCs)
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 - A WG (single)
Central Maintenance Computer - CMC (single)
4-Axis 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 YOR/LOC/GS/MB
One ADF
One DME
Two pedestal mounted MCDU (Multi - Control Function Display Units)
1st Radar Altimeter (RT-300)
2nd Radar Altimeter System (RT-300) Emergency Locator Transmitter
One Flight Guidance Controller
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 (CYR/FDR) with Underwater Locator Beacon (ULB)

Additional Installed Equipment

Passenger cabin hinged doors (RH and LH)
“Roundy” Cabinet + Entertainment package (including CD/DVD player; 2 display 17” LCD) + Jet map
Customized painting scheme
Main rotor blades high visibility painting
Approach plates chart holders with lights for pilot and co-pilot
Windshield washing system
5th display in cockpit (stand-alone)
ADF 2nd unit (Fully installed)
Auxiliary heavy duty battery 27 Ah (in lieu of 13 Ah)
Enhanced Ground Proximity Warning System (EGPWS) (provision & removable)
GPS, 2nd (provision and removable)
HF/SSB Transceiver Primus HF- I 050 Honeywell provision
Moving Map EuroNav V with standard aeronautical charts provision
Moving Map EuroNav V (stand-alone) with standard aeronautical charts (removable)
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 removable
Additional anti-collision light under fuselage
Anti-icing system/combined accessory gear box
Auxiliary transversal fuel tanks 132 USG provision
Auxiliary transversal fuel tanks 132 USG removable
Emergency floats provision
Increased gross weight - 6.800 kg
Life rafts (Qty 2) up to 17 passengers each provision
Snow skids/slump protection pads provision
Anti sinking pads removable (tow bar adapter included)
Wire strike protection system
SATCOM Aircell 3100
Russian certification 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 mam rotor blades (5)
Tail rotor: blades flapping block (1)
Main rotor blade 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)

Interior & Cabin Equipment

Pilot/ and co-pilot 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 sunshades
Fluorescent lighted emergency exit signs
Cockpit map and data case in central console
Two flashlights 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

Five Stars Cabin Basic Arrangement, Including

Conversion kit for 8 passengers
2 armchairs leather covered (with inertial reels sliding inflight direction, reclining backrest and separate 4 points safety belts)
Comfortable seat leather covered (with safety belts and under- seat skirts) (Qty 4)
Armrests leather covered for comfortable seats fwd. (Qty 3)
Lateral armrest-cabinets leather covered with metal cup holder (Qty 2)
Headsets Bose ANR type (Qty 6)
Fashion cabinet with newspaper holder and air conditioning control panel
Multipurpose Cubby with 3 sliding doors
Separation wall leather and leatherette covered with manual sliding window and roll up curtain on pilots side
Super Silent soundproofing
Electrically operated pax steps (RH and LH)
Nose landing gear doors • Customized VIP cabin finishing
Decoration trim
Passenger carpet (high thickness)
Air conditioning system
P.A. (Passenger Address) system (including loudspeakers and safety belts lights)
JCS in the cabin for all passengers
Passenger cabin thermo acoustic tinted double layer windows
Hydraulic pulsation dampeners
Active Vibration Control System Provision & Removable (AVCS)
MGB Premium Grade
Cyclic and collective leather gators (same colour as cabin interior)
Cabin vertical handles metal finished on doorposts (Qty 2)
Alternate Current (AC) power outlet (28V)
Coat Hooks (Qty. 4)

Printing

Standard colour scheme from HeliVert paint selection, solid colour

Specifications are subject to verification by purchaser upon Inspection. Aircraft is subject to prior sale and/or removal from the market without prior notice.