2019 AgustaWestland - AW109
  • Aluminium alloy and bonded panel fuselage
  • Semi-monocoque aluminium alloy tail boom
  • Three wheel retractable landing gear
  • Two hinged jettisonable high crew doors (LH & RH)
  • Two sliding passenger doors (LH & RH), 1.40 m opening, with jettisonable windows
  • Acrylic windshield and side windows
  • Acrylic transparent overhead windows
  • Quick removable tail rotor drive shaft cover
  • Separate baggage compartment with hinged door
  • Removable fairing and cowlings,for complete accessibility to the controls and drive components
  • Swivelling front wheel provided with tow bar attachment
  • Quick opening hinged inspection doors to allow visual check of engine oil levels and maintenance inspection points
  • Grounding points
  • Jacking and hoisting points
Rotors & Controls
  • Titanium metal main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite blades, swept tips, and dampers.
  • Steel metal 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
Transmission / Drive System & Hydraulic System
  • 960 shp for take-off and 900 shp continuous operation main transmission
  • Three stage transmission
  • Two free wheeling units
  • Dual independent, redundant hydraulic systems
  • Two transmission mounted hydraulic pumps with separate reservoir
  • Ripple dampers(2)
  • 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
Electrical System
  • 24 V DC 33Ah nickel cadmium battery (19 cells) with temperature probe
  • 200 A self cooled starter generators (2)
  • Voltage regulators (2)
  • Battery relay
  • Interconnecting bus relay (2)
  • External power relay
  • Distribution buses (1 battery, 2 essential, 2 EMER, 2 main, 2 auxiliary)
  • External power receptacle
  • Position lights( NVG friendly -green,red,white)
  • Taxing lights (2RH+2LH) and landing lights (2RH+2LH) on landing gear sponsons
  • Anti collision lights (2) ( NVG friendly )
  • Utility cockpit lights (2)
  • Instrument lights with dimming switch
  • Radio master switch with ground function
Flight / Navigation Instruments
  • Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP)
  • Radio Management System (RMS) RTU-4210 Collins (1)
  • VHF/AM VHF-4000E
  • VOR/ILS NAV-4500 Collins
  • Transponder (Mode S) TDR-94 Collins
  • Attitude Heading Reference System (AHRS) (1) with one dual AHRS control panel
  • Air Data Unit (ADU)
  • Digital Audio Control System (DACS) COBHAM with one cockpit panel
  • Electronic clock (1)
  • Magnetic compass indicator (1)
  • Magnetic sensor unit
  • Pitot tube right/left
Instrumentation (on IDS Displays)
  • LCD integrated display system (IDS)
  • Dual gas generator speed (N1%)
  • Dual turbine outlet temperature (TOT °C)
  • Dual torque meter (TQ%)
  • Dual power turbine speed (N2%)
  • Rotor speed (NR%)
  • Transmission oil temperature (°C) and pressure Indicator (PSI)
  • Two engine oil temperature (°C) and pressure Indicator (PSI)
  • Two fuel pressure Indicator (PSI)
  • Two fuel quantity Indicator (kg)
  • Two fuel flow Indicator (kg/hr)
  • Two flight controls hydraulic system pressure Indicator (PSI)
  • Two utility hydraulic system pressure Indicator (PSI)
  • Outside air temperature Indicator (°C)
  • 2 DC ammeter
  • 2 DC voltmeter
  • 2 AC voltmeter
Warning, Caution & Advisory System
  • Master Warning Lights (2)
  • Master Caution Lights (2)
  • Warning, caution & advisory messages (on IDS display)
  • Aural Warning Generator system
  • Engine fire detection system
  • Exceedance recorder system (on IDS display)
  • Warning horn (cabin)
Interior Arrangement
  • Crash-resistant pilot seat, fore and aft adjustable, with lap belts and headrests
  • Aluminium alloy honeycomb reinforced floor with anti skid finish
  • Ventilation ram air inlets
  • Anti reflection instrument panel
Exterior Finishing
  • Finishing in accordance with manufacturer specification (NTA 893 A)
  • Primer exterior painting
Standard Equipment
  • Active Noise Reduction (ANR) headsets (pilot and co-pilot)
  • Baggage compartment lights
  • Crash-resistant co-pilot seat, fore and aft adjustable, with lap belts and headrests
  • Crew open door actuators
  • First aid kit
  • Fuel drain electrical valves
  • Internal structural provisions for utility equipment
  • Portable fire extinguisher
  • Shoulder harness with inertial reels(pilot and co-pilot) 
  • Tail boom strake
Single Pilot Dual Controls IFR Avionic Package
  • Pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP) (*)In lieu of basic pilot flight/navigation EFIS(1display) with slip indicator and romote bug panel(RBP) (**) Data services subscription for the update of the navigation databases from Jeppesen is under customer’s responsibility.
  • Co-pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP)
  • Reversionary Control Panel (RCP)
  • EFIS pilot/co-pilot navigation synchronization switch (FMS data)
  • Electronic Standby Instrument System (ESIS)
  • Second Radio Management System (RMS) RTU-4210 Collins
  • Second VHF/AM VHF-4000E Collins
  • VOR/ILS/ADF NAV-4000 Collins
  • DME DME-4000 Collins
  • Radio altimeter ALT-4000 Collins
  • Second Attitude Heading Reference System (AHRS)
  • Second Air Data Unit (ADU)
  • Pilot GPS/SBAS Chelton interfaced to EFIS/FMS
  • Co-pilot GPS/SBAS Chelton interfaced to EFIS/FMS 
  • Digital Audio Control System (DACS) COBHAM additional cockpit panel
  • 4-axis dual duplex digital AFCS with integrated Flight Director
  • Second electronic clock
  • Second magnetic compass indicator
  • ELT C406-N HM Artex (with Navigation Interface Module embedded)
Additional Equipment
  • Airframe hour meter
  • Baggage compartment extension (1.9 m) (*) It may be affected by avionic customization.
  • Engine compartment fire extinguishers (Qty 2)
  • Fuel cap with key-lock
  • Pulsed chip detectors (in lieu of quick disconnecting chip detectors)
  • Reinforced windshields
  • Retractable/rotating landing light (nose mounted)
  • Rotor brake
  • Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
Interior Trim
  • Air conditioning ECS (Environment Control System)
  • Primer finished cabin walls
  • Standard colour scheme from Company paint selection, solid colour
Interior Equipment Cabin
  • 0P-A-040-3CM Utility interior
  • Passenger cabin
  • All seats crash-resistant covered with leatherette
  • 3 fwd facing seats (aft bench) with seating modules individually removable
  • 3 aft facing seats (central bench) with seating modules individually removable
  • 4-point shoulder harness with inertial reels and safety belts for all seats
  • Light soundproofing
  • Painted liners
  • Intercommunication system for passengers
  • Cabin loudspeakers (Qty 2)
  • Reading lights, emergency lights
  • Upper and lower air vents
  • Headset Bose ANR type (Qty 6)
  • Cockpit equipment
  • Standard cockpit interior
Avionics Equipment
  • 3rd ICS station in passengers cabin
  • 8.4” cockpit central display
  • Cockpit Voice / Flight Data Recorder (CVR/FDR) Penny & Giles (*) Requires cable/software available as GSE”
  • Weather radar RDR 2000 Bendix/King (presented on EFIS)
  • HD Video Recorder Aero-Optical HD-HCAR-C (integrated in the mission console)
  • Police radio (350 MHz PDT Radio Hytera MD780G) full provision. (*) Police radio shall be a customer furnished equipment (CFE).
Utility Equipment
  • Cargo hook (1150 kg) provision (*) Requires either the rear mirror or the cargo hook camera
  • Cargo hook / cargo cameras (*) requires the installatation of 8.4’’ display
  • External loudspeakers (250 W) provision
  • External rescue hoist (272 kg/600 lb) (Goodrich) provision including step bar
  • Rappelling hooks (2 LH+2 RH) including step bar (LH) (ropes excluded) (*) requires the installatation of the RH step bar
  • Searchlight SX-16 Nightsun provision RH side nose installation
  • Searchlight SX-16 Nightsun FLIR slaving unit
  • FLIR Ultraforce 350 HD provision
  • Floor rails
Finishing Painting
  • AgustaWestland painting scheme, metallic colours from Company selection
Removable Equipment
  • 177 USgal crash-resistant fuel system (in lieu of 152 USgal) (*) Not compatible with dual stretcher installation.
  • Cargo hook (1150 kg) removable
  • External rescue hoist (272 kg/600 lb) (Goodrich) removable with single control pendant
  • Wireless ICS Polycon System (UHF) (*) Required for Human External Cargo (HEC) operations
  • External loudspeakers (250 W) removable
  • Searchlight SX-16 Nightsun removable RH side nose installation
  • FLIR Ultraforce 350 HD removable (includes Turret with quick disconnect, MWIR Camera, Daylight TV camera and Hand Control Grip on Mission Console)
  • Mission console in cabin with 17” HD display (in lieu of central bench)
  • Digital video downlink (Sino Flying Video Hi-Tech Limited) full provision[1] (*)System shall be a customer furnished equipment (CFE).
  • Beidou/GPS full provision (*)System shall be a customer furnished equipment (CFE).
Specifications are subject to verification by purchaser upon Inspection. Aircraft is subject to prior sale and/or removal from the market without prior notice.