HZ-AC32 - 2010 AGUSTA AW139

2010

AGUSTA

AW139

31290

HZ-AC32

Used

We are selling 20 helicopters (6 Agusta 109E and 14 Agusta AW139) as well as an extensive list of A109 spare parts for one owner in a tender. For picture specs, component times and further technical info, please visit:

10345

Airframe Aluminium alloy fuselage Glass Windshields Overhead cockpit windows Lower cockpit 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) Failure warning (2) One cockpit and one pilot cabin fire extinguisher Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side) Plug in sliding doors (2) for passenger cabin access with four locking latches Six cabin push-out emergency exit windows (two on each passenger cabin door) Baggage compartment with 2 lockable baggage compartment doors, LH & RH side Baggage compartment cargo tie-down fittings Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear) Strucutral provisions for nose landing gear doors Landing gear mooring Upper deck mooring provisions 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 Electrical System DC primary power generation: 28V DC regulated voltage provided by two independent 300A starter generators DC External Power Receptacle Two Nickel-Cadmium Batteries: one 40Ah main battery plus one 13 Ah auxiliary battery 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) Rotating/retracting landing light Baggage compartment lighting (3) and smoke sensor

Rotors and Controls Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers Rotating M/R flight controls Main rotor hub beanie Three main dual servo actuators Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers Rotating T/R 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) Chip burning capability for intermediate and tail rotor gearboxes

Two Pratt & Whitney Canada PT6C-67C engines Two independent FADEC systems (one on each engine) 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) Engine exhausts and ejectors Two independent crashworthy fuel cells Two supply pumps on engines Two booster pumps submerged in fuel tanks Two fuel filter assemblies Two engine back-up controls, mechanical and electrical Two manual engines start and ingnition system Engine chip detectors, with chip burning capability

Additional Installed Equipment Air Conditioning Approach plates chart holders lighted for both pilot/co-pilot Emergency floats removable parts Life Rafts (2) up to 17 passengers each External loudspeakers provisions & installation Auxiliary fuel tanks provisions Cup holders for both pilot/co-pilot Weather/search radar Honeywell Primus 701 provisions including AC inverter & weather/search radar Honeywell Primus 701 Flexcomm II multiband radio V/UHF RT5000 provisions Flexcomm II multiband radio V/UHF RT5000 system HUMS (Health & Usage Monitoring System): -Structural / electrical provisions -Fixed Parts (sensors I accelerometers I velocity sensors) -Removable Parts (computer control boxes+ control panel+ rotor track & balance sensor) -Ground station {Laptop+ Software+ License) TCAS I provision TCAS I Bendix King (KTA-970 model) HEELS (Helicopter Emergency Exit Lighting System) ADELT (Automatic Deployable ELT w/ Nav interface) Tinted overhead Cockpit Window Storm Window (Co-Pilot) ICS 12 Pax 12 Pax Headsets Std. David Clark H10-13H Cabin tinted windows 2nd refueling point and protection plates (1 point close circuit) High visibility main rotor blades Hydraulic pulsation damper 4-Axis Digital Automatic Flight Control System – DAFCS (add. To std. 3-axis) EGPWS (Enhanced Ground Proximity Warning System) provisions EGPWS (Enhanced Ground Proximity Warning System) full kit Medevac kit 4 places provisions Improved additional soundproofing Enhanced Vision System EVS-1000 Additional anti-collision light P.A. System PBS 250 Pilot/Co-Pilot adjustable seats in lieu of standard seats Cargo Net in Baggage Compartment and Cargo Tie Down Fittings Nose Landing Gear Door Provision for VIP Interior HUMS FLOATS & Life RAFTS Kits EGPWS KIT (enhanced ground proximity warning system) TCAS (Traffic alert collision avoidance system) MAX VIZ Camera Kit Loudspeaker Kit Weather Radar Kit Primus 701 V/UHF Flexcomm 2 Kit Kit 5 Display Kit 2nd ADF Fin Camera Kit List of Supplements Emergency Floats Control Panel relocation on inter seat console Increase of Aircraft Maximum Take Off Weight (MTOW) up to 6800kg Mast Vibration Absorber Kit P/N 4G1860f00113 Installation of Power Parking Brake Module, Kit P/N 3G3240f00111 STC- Installation of AFS Inlet Barrier Filter System Installation of Lifeport Dual Litter System Ceiling liner split retro-modification P/N 3G2506P07812 Quick Access Recorder Kit P/N 4G3130F00411 Installation of Instrument Panel Improved Fixing Supports Installation of Additional Cowling latches Kit P/N 4G7110F00111 Modification of Engine Exhaust Pipe Fairing 3rd Mass Vibration Kit P/N 3G1860F00111 List of Supplemental Type Certificates STC – Installation of Cargo/Cabin floor Protector Kit – Dart STC – Installation of AFS Inlet Barrier Filter System

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" 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" color 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 (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 (RICs) 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-AWG (single) -Central Maintenance Computer-CMG (single) -3-Axis Digital Automatic Flight Control System - DAFCS (dual) with auto-trim function -Provision for CVR/FDR data interface (single) -Flight Director System (dual) Pilot and co-pilot microphone and headset 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 pedestals mounted MCDUs (Multi Control Function Display Units) 1st Radar Altimeter (RT-300) 2nd Radar Altimeter System (RT-300) Emergency Locator Transmitter (EL T -121.5/243/406 MHz) 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) One magnetic compass One Outside Air Temperature indicator Two Master Warning Lights (MWLs) Two Master Caution Lights (MCLs) Engine 1 Fire Light Engine 2 Fire Light Baggage compartment smoke detector light Dual electricalpower connection for CVR/FDR (FAA requirement compliant) Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)

Helicopter‘s additional equipment (exceeding fleet configuration): SKYTRAC ISAT-100

Polyurethane painting in accordance with AgustaWestland standard painting scheme

Cabin, cockpit and baggage compartment utility finishing interior Pilot/ 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 sun shades Floor provisions for 15-seat configuration Fluorescent lighted emergency exit signs