2018 LEONARDO AW139

2018

LEONARDO

AW139

New

IFR

Brand New AW139 for VIP and offshore mission available for sale!Delivery immediately !

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AW139 Baseline Aircraft Airframe Aluminium alloy fuselage Acrylic windshields Overhead cockpit transparent windows Lower cockpit transparent windows Lower pilot & co-pilot door windows Cockpit ram air adjustable outlets 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 passenger cabin access with four locking latches and additional sliding doors cabin handle (2 - one on each side) 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) 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 Horizontal 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 Adaptive Anti Vibration Control System with rotational damping masses - Utility 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 Main dual servo actuators (3) Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four fully 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 Provision for main rotor tracking (magnetic pick-up) Power Plant and Fuel System 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 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 gauge and magnetic drain plug/chip detector Dual independent, redundant hydraulic systems Two hydraulic Power Control Modules (PCM) 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 (20 cells) 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) Retractable/rotating landing/taxing lights (2) Baggage compartment lights (3) and smoke sensor Standard Avionic Package 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

AW Premium Equipment Forced fan ventilation Bleed air heater and deforster with air noise suppressions Cockpit air ventilation system Baggage compartment cargo tie-down for increased load capacity(up to 300KG) Rotor brake 1st radar altimeter RT-300 2st radar altimeter RT-300 4-axis dual digital automatic flight control system(DAFCS) Basic incorporated into Modular Avionics Units(MAUs) Flight Director System (Dual) incorporated into the Modular Avionics Unites(MAU) Two Honeywell GPS modules with Flight Plan Management System(FPMS) One Model S diversity transponder with Extended Squitter (ADSB-Out 1090MHz) incorporated into the Modular Radio Cabinet(MRC) Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon(ULB) Health & Usage Monitoring System (HUMS) Increased Payload Package Increased Gross Weight - 6,800 kg PROPOSED CONFIGURATION Interior Equipment - Cabin "Utility/Passaenger cabin basic arrangement - soundproofing -Standard roof liner with dome lights -Polycarbonater liner -Rubber carpet - P.A. (Passenger Address) system (with loudspeakers) on std ICS - Fixed steps for passenger cabin access (LH and RH)" "12 seats interior layout -12-padded lightweight crashworthy seats fabric cover(with 4-point shoulder hamess with internal reels safety belt)disposed on 3 rows" Avoinics Equipment Enhanced Ground Proximity Warning System(EGWPS) Provision Enhanced Ground Proximity Warning System(EGWPS) removable ADELT (2-frequency Automatic Deployable ELT w/ GPS interface) (*) In liieu of standard ELT TCAS I KTA-970 Honeywell Bendix/King provision "TCAS I KTA-970 Honeywell Bendix/King removable (*) Required for VFR night single pilot operations." Weather Radar Primus 660 Honeywell provision Weather Radar Primus 660 Honeywell removable Utility Equipment Emergency floats provision Emergency floats removable Life rafts up to 14 passengers each provision (Qty 2) Life rafts up to 14 passengers each removable(Qty 2) Auxiliary transversal fuel tank 132 USgal provision Auxiliary transversal fuel tank 132 USgal removable Mission Equipment Increased Gross Weight - 7000 kg Finishing-Painting AgustaWestland painting scheme, metallic colours from Company selection Optional Equipment Interior Equipment - Cabin Air conditioning system Interior Equipment - Cockpit "Cockpit tinted upper window (*) Smocked colours" Utility Equipment External louderspeakers(400W) Provision External louderspeakers(400W)removable "Rescue hoist (Goodrich) provision - single type (*) Including ICS AV900 Honeywell, wireless ICS Polycon and swivelling light for rescue hoist (belly mounted)" Rescue hoist (Goodrich) removable - single type Maritime protection Mission Equipment Aerolite single stretcher(installed transversally)