Leonardo AW139

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)

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

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

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

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, with chip burning capability.
Tail gearbox with sight gauge and magnetic drain plug/chip detector, with chip burning capability
Dual independent, redundant hydraulic systems
Two hydraulic Power Control Modules (PCMs)
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

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


Miscellaneous
Manuals, aircaft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue
Tie down-assemblies for amin rotor blades (5)
Main landing gear wheel chocks (2)
Nose landing gear canter pin (1) and landing gear handle locking pin (1)

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

Polyurethane painting in accordance with AgustaWestland standard painting scheme

Helicopter‘s additional equipment (exceeding fleet configuration):
Rescue Hoist Provisions
Night Sun II XP Search Light provision
Wescam MX-15I FLIR provision
Cargo hook provision
5th Display on Instrument Panel
Digital Video Recorder (provision)
Rescue Hoist Goodrich Provision
SAT-Com Flight Deck Sky Connect

List of Supplements (exceeding fleet configuration):
Quick Disconnect Modification on Cabin ICS Headset-to-Roof
Relocation of HEELS BT7 Battery (BT 139-178)
SAR MODIFICATION (Primus Epic 5.6, PAX footstep extension, cockpit NVG, 2nd GPS, Epic, SAR MODE, Windshield Wiper

List of Supplemental Type Certificates (exceeding fleet configuration):
STC – Skytrac ISAT-200A
STC – Night Vision modification (Aviation Services Unlimited – ASU)

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

Date of Phased Out: 2020-04-30

Once helicopter was parked, basic preservation was performed including preservation fluids, oils, etc. Parts were removed to prevent from doing work such as turning the engines or the gear box etc.. No further action has been done since then.

These particulars have been prepared by Avionmar from information provided by the sellers and are intended as a general guide to the aircraft. Avionmar cannot, however, be liable for any inaccuracy. Avionmar strictly advises any purchaser to check the current and remaining hours themselves in the provided document “Aircrafts – Planner Board”. It is up to the purchaser to confirm details of concern to him by survey, inspection and/or enquiry of the seller and to ensure that the purchase contract properly reflects his concern and specific details upon which he may rely. AvionMar always advises an independent survey.