2018 阿古斯特 韦斯特兰 - AW119 MK II SN14953
Aircraft
  • Manufactured Year: 2018
  • Serial Number: 14953
  • Total Hours: 250 Hours
  • Asking Price: Make offer
Aircraft Highlights
  • EMS Configuration / 2+8 Seating Convertible 
  • Single Pilot VFR Configuration (FAA/EASA Standard)
  • MTOW Load 2850kg Internal, 3150kg External
  • Single Stretcher - Removable Parts 
  • Air Conditioning 
  • 188 Gal Fuel System Upgrade
  • Oxygen Bottle in Baggage Compartment
  • Two Hinged Jettisonable Crew Doors & Two Sliding Passenger Doors
  • Garmin G1000H Integrated Flight Deck System
Avionics
Garmin G1000H Integrated Flight Deck system comprising:
  • Two GDU-1040 10.4" display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating: 
  • Radio tuning controls
  • Flight Management System (FMS) 
  • Synthetic Vision System 
  • Helicopter Terrain Awareness and Warning System (HTAWS) 
  • Two GEA-71H Aircraft Interface Unit with integral Central Maintenance Computer (CMC) 
  • Two GSC-46 Signal Conditioners
  • GRS-77H AHRS
  • GDC-74H Air Data Computer (ADC)
  • Two GIA-63H Integrated Avionics Units (IAU) comprising: COM 1&2 / NAV 1&2 / GPS 1&2 / Aural Alert Generator / DME tuning interface
  • GTX-33H Mode-S Transponder with Extended Squitter (ES) capability 
  • Radar Altimeter RA-4500 FreeFlight Systems 
  • Digital Audio Control System (DACS) NAT with two cockpit panels
  • Magnetic Compass indicator 
  • L3 Avionics System ESI-2000 Electronic Standby Indicator
  • Airframe Hour meter
Engines
Engines Model: PT6B-37A
  • Total Hours: 250 Since New
Airframe
  • Aluminium alloy and bonded panel fuselage
  • Semi-monocoque aluminium alloy tail boom
  • New reinforced skid type landing gear
  • Two hinged jettisonable crew doors (LH & RH)
  • Two sliding passenger doors (LH and RH), 1.10 m opening, with jettisonable windows
  • Passenger short foot step (LH & RH)
  • Acrylic windshield and side windows
  • Overhead cockpit transparent windows
  • Lower cockpit transparent windows
  • Removable fibreglass tail rotor gearbox fairing
  • Quick removable tail rotor drive shaft cover
  • Separate baggage compartment with hinged door
  • Three jacking points 
  • Removable fairing and cowlings, for complete accessibility to the controls and drive components
  • Quick opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points
  • Grounding point
Transmission drive system & hydraulic system
  • 917 shp for takeoff and 900 shp continuous operation main transmission
  • Two-stage transmission
  • Transmission mounted hydraulic pumps (2) with separate reservoir
  • Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter
  • Transmission oil chip detectors (2)
  • Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detector
  • Transmission cooling and lubrication system 
  • Transmission shafts
Rotors and Controls
  • Titanium main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite material blades, swept tips, and dampers
  • Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite blades, individually interchangeable
  • Cyclic and collective controls powered by two hydraulic systems
  • Hydraulically powered anti-torque system
  • Adjustable friction devices on cyclic and collective system 
  • Force trim and artificial feel system
  • Adjustable directional control pedals
  • Flapping and droop restraint mechanism
Electrical Systems
  • 28 V DC 22 Ah nickel-cadmium battery with temperature probe
  • 200 A self-cooled starter generator
  • Voltage regulator
  • Battery relay
  • Interconnecting bus relay
  • External power relay
  • Distribution buses (2)
  • External power receptacle
  • Position lights
  • 250 W landing lights (2)
  • Anti collision lights (2)
  • Cockpit utility lights (2)
  • Instrument lights with dimming switch
  • Radio master switch
Central Warning System (CWS)
  • Master warning lights
  • Master caution lights
  • Warning, caution and advisory messages on PDF display
  • Aural alerts from IAU 1 & 2
System Data (On MFD/PFD)
  • Inter turbine gas temperature indicator (ITT°C)
  • Engine torque indicator (TQ%)
  • Compressor speed indicator (N1%)
  • Turbine speed indicator (N2%) 
  • Rotor speed indicator (NR%) 
  • Transmission oil pressure (PSI) and temperature (°C) indicator (on MFD)
  • Engine oil pressure (PSI) and temperature (°C) indicator (on MFD)
  • Fuel pressure (PSI) (on MFD) and fuel quantity (kg) indicator (on PFD/MFD)
  • Two hydraulic pressure system indicators (PSI) (on MFD) 
  • Outside air temperature indicator (°C) (on PFD) 
  • DC voltmeter (VDC) (on MFD)
  • DC ammeter (Amp) (on MFD)
Miscellaneous / Ground Equipment
  • Air intake/exhaust covers
  • Ground tools kit (including tow bar, ground wheels, lifting tool)
  • Pitot tube cover
  • Rotorcraft Flight Manual (RFM) and technical publications 
  • Tie-down fitting (main rotor and tail rotor retention straps)
Interior
  • Pilot and co-pilot seats, fore and aft adjustable, with lap belts and headrests
  • Aluminium alloy honeycomb reinforced floor with anti-skid finishing
  • Ventilation ram air inlets
  • Anti reflection instrument panel
Exterior
  • Finishing in accordance with manufacturer specification (NTA893A)
  • Primer exterior painting
Specifications are subject to verification by purchaser upon Inspection. Aircraft is subject to prior sale and/or removal from the market without prior notice.