2019 AgustaWestland - AW139
  • Aluminium alloy fuselage
  • Acrylic windshields
  • Overhead cockpit transparent windows
  • Lower cockpit transparent 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
  • 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
  • Anti Vibration masses (2)under cabin floor
  • Lower pilot & co-pilot door windows
  • Additional sliding doors cabin handles (2-one on each side)
  • “Adaptive Anti Vibration Control System with rotational damping masses - Utility (*) In lieu of Anti-vibration masses (2) under cabin floor”
  • “Four fully elastomeric tail rotor damper (*) In lieu of four elastomeric tail rotor damper”
  • Health & Usage Monitoring System (HUMS)
  • Increased Gross weight-7000Kg
Rotors & 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)
Transmission drive system & 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
Power Plant & 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
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 Control Devices (CCD)
  • One Reversion Control Panel (RCP)
  • One Display Dimming Control Panel (DCP)
  • One Stability Augmentation System (SAS) control panel
  • Two Remote Instrument Controllers (RIC)
  • Two Modular Avionic Units (MAU) 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 (CMC) single
- Provision for CVR/FDR data interface (single)
  • 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.
  • Right Modular Radio Cabinet (MRC) with the following modules:
- One VHF Comm.
- One ADF
- One DME
  • Two pedestal mounted Multifunction Control Display Units (MCDU)
  • Emergency Locator Transmitter (ELT)
  • One flight guidance controller
  • 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)
Miscellaneous / Ground Equipment
  • Cargo net in baggage compartment for increased load capacity (up to 300 kg)
  • 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 main rotor blades (5)
  • Tail rotor blades flapping block (1)
  • Main rotor blades 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)
Electrical System
  • DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators
  • DC external power receptacle
  • wo 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
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
  • 2nd 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 (GNSS/SBAS) modules with Flight Plan Management System(FPMS)
  • One Model S diversity transponder with Extended Squitter (ADS-B Out 1090MHz) incorporated into the Modular Radio Cabinet(MRC)
  • Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon(ULB)
  • Standard colour scheme from Company paint selection, solid colour
Exterior Finishing
  • Customised painting scheme, metallic colours from Company selection
  • Pilot and co-pilot crashworthy seats (with inertial reels and safety belts)
  • Cockpit dome/storm light
  • Cockpit utility lights (2)
  • 28 V DC cockpit/cabin power outlet
  • Cockpit panel sun-glare shields
  • Overhead cockpit windows sun shades
  • Fluorescent emergency exit signs
  • Cockpit map and data case in central console
  • Two flash lights for pilot and co-pilot
  • ICS panel with plug for one headset (LH side)
  • First aid kit
Interior Equipment Cabin
  • Law Enforcement cabin basic arrangement
– Soft liners
– Cabin emergency lights
– Cabin loudspeakers
– Cargo net between baggage and cabin compartment(loose equipment)
– Dome lights
– Fixed steps for passenger cabin access (RH and LH)
– Floor and ceiling provision for foldable seats installation
  • Air conditioning system
  • Foldable passenger seat (10) (*) 5+5 back-to-back interior layout is company qualified.
Interior Equipment Cockpit
  • Co-pilot hinged window (storm window)
  • Pilot headset hooks (Qty 2)
  • “Approach plates chart holder with lights for pilot and co-pilot (*) required for single pilot IFR operations.”
Avionics Equipment
  • 4-axis DAFCS enhanced with hover mode
  • Auxiliary heavy duty battery 28 Ah ( In lieu of 13 Ah)
  • Digital Video Recorder Aero Optical DVFAR-II
  • ICS AV900 Honeywell-2 headset plugs for cabin operator (*) 4th station
  • ICS GEM-05 Gemelli-8 headset plugs (1)
  • 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
  • Police radio 350 MHz PDT Radio Hytera MD780G provision (*)Police radio shall be a customer furnished equipment(CFE)
  • Headset H10-13H David Clark (QTY2)
  • Pilot helmets(QTY3) (*) Gallet LH350
Utility Equipment
  • Bambi bucket (up to 2,000 lt/530 USgal – 2,085 kg/4,587 lb) provision
  • Cabin extension for baggage accessibility
  • Cargo hook (2,200 kg/4,850 lb) provision (*)Including cargo hook monitoring cameras provision
  • Cargo hook (2,200 kg/4,850 lb) removable (*)Including cargo hook monitoring cameras(Qty 2)
  • External louderspeakers(700W) Provision
  • External louderspeakers(700W)removable
  • Rescue hoist (Goodrich) provision - single type (*) Including ICS AV900 Honeywell, wireless ICS Polycon and swivelling light for rescue hoist • Rescue hoist (Goodrich) removable - single type
  • Wire strike protection system (*) Lower cutter blade is not install when FLIR system is selected.
  • Search Light Trakkabeam A800 provision
  • Search Light Trakkabeam A800 removable
  • Auxiliary longitudinal (LH) fuel tank 132 USgal provision
Mission Equipment
  • Fast roping and rappelling system foldable (LH and RH) provision
  • Fast roping and rappelling system foldable (LH and RH) removable(*)Company qualified
  • Mission Console in passenger cabin provision(21.5’’HD display) (*) Including Video Management System
  • Ice detector system
  • SAR handle on the doorpost(qty 2)
  • FLIR Ultra Force 350 HD provision
  • FLIR Ultra Force 350 HD removable (*)including Turret with quick disconnect, MWIR Camera, Daylight TV camera and Hand Control Grip on Mission Console)
  • Beidou/GPS provision
  • Digital downlink system provision (*) On-Helicopter system/Sino Flying video Hi-tech Limited(1.4GHz)(**) Removable, Fixed and portable receiving stations are customer Furnishd Equipment(CFE). • Mission console in passenger cabin removable(21.5’’HD display)
Self-Contained EMS KITS / MEDVAC Systems
  • Aerolite dual stretcher(installed transversally)
Specifications are subject to verification by purchaser upon Inspection. Aircraft is subject to prior sale and/or removal from the market without prior notice.