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2009 Agusta AW139
Starts from the median asking price of 476 comparable Helicopter listings ($459,677), then adjusts for:
- Year +1 vs comparable listings +1.5%
- Airframe time +566 hr vs comps -1.1%
Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.
Overview
| Make / Model | Agusta AW139 |
|---|---|
| Type | Helicopter |
| Airframe time | 2,164 hrs |
Description
2009 Agusta AW139 is an active turbine helicopters listing on Aircraft Shopper Online. Aircraft location: Canada. Listed by Aero Asset Inc. Total time: 2,164 ho
Modifications
Back 20 Photos Price on request: Make Offer (Strictly for Sale) 2009 Agusta AW139 S/N: 31239 R/N: F-HHJM 2,164 Total Hours Canada Compare Date Listed: May 19, 2026 Seller Paragraph Seller Aero Asset Inc Location Toronto, CA New ‘FiveStar’ VIP interior & paint @ Leonardo in 2022 6.8T MTOW, Avionics ph7 EAPS, floats, aux tanks, AVCS Fresh 4 yr inspection @ Leonardo Hangared Paris, France Click here for Virtual 3D Tour Airframe & Power Systems Information Notes Status as of (May 13, 2026) Engines Loc. Make Model Serial# TSN L Pratt & Whitney PT6C-67C PCE-KB0513 2,164 R PCE-KB0493 2,164 Airframe Notes Status as of (May 13, 2026) 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 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 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 Engine Type Pratt & Whitney PT6C-67C Engine Count 2 Engine Hours 2,164 hours Propeller Count 1 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 27 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 Light Baggage Compartment Lights (3) and Smoke Sensor Avionics 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. One VOR/LOC/GS/MB Right Modular Radio Cabinet (MRC) with the Following Modules: One VHF COMM. One VOR/LOC/GS/MB 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) AW Premium Equipment Forced Fan Ventilation Bleed Air Heater and Defroster with Air Noise Suppressions Cockpit Air Ventilation System Baggage Compartment Cargo Tie-down Fittings 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 Avionic Units (MAUs) Flight Director System (dual) Incorporated into the Modular Avionic Unit (MAU) Two Honeywell GPS Modules (GNSS/SBAS – Global Navigation Satellite System/Satellite Based Augmentation System) with Flight Plan Management System (FPMS) One Mode S diversity transponder with Extended Squitter (ADSB-Out 1090 MHz) incorporated into the Modular Radio Cabinet (MRC) Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB) Miscellaneous / Ground Equipment Cargo Net in Baggage Compartment Covers and Flags: Engine Exhaust Pipes (2), Engine Air Inlets (2) and Pitot Tubes (2), Manuals: 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) Tow Bar Loose Equipment Bag (1) Mission Equipment Increased Gross Weight - 6,800 Kg (14,991 lb) Approach Plates Chart Holders with Lights for Pilot and Co-pilot Pilot and Co-pilot Adjustable Seats (in lieu of standard seats) Heated Glass Windshield 4-Axis DAFCS (Digital Automatic Flight Control System) Enhanced with Hover Mode (HOV) Enhanced Ground Proximity Warning System (EGPWS) Provision Enhanced Ground Proximity Warning System (EGPWS) Removable 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 Removable Weather Radar Primus 660 Honeywell Provision Lightning Sensor System Honeywell LSZ-860 5th Display in Cockpit ADELT (2-frequency Automatic Deployable ELT w/ GPS interface) (*) In lieu of standard ELT Moving Map Euroavionics EuroNav V - Provision Moving Map Euroavionics EuroNav V – Removable Auxiliary Transversal Fuel Tank 132 USgal - Provision Auxiliary Transversal Fuel Tank 132 USgal - Removable Emergency Floats Provision Emergency Floats Removable Emergency Floats Kevlar Covers Engine Air Particle Separator (EAPS) - Provision Engine Air Particle Separator (EAPS) – Removable Ice Detector System Interior Standard Interior 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 Map and Data Cases in Pilot and Co-pilot Doors ICS Panel with Plug for One Headset (LH side) First Aid Kit VIP Interior 'FiveStar' Interior Layout - 7 Seats 3 Armchairs Leather Covered (with inertial reels, sliding inflight direction, reclining backrest and separate 4-point safety belts) Comfortable Seat Leather Covered (with safety belts and under-seat skirts) (Qty 4) Multipurpose Cubby with Sliding Doors Passenger Cabin Hinged Doors Including: Extra Silent Soundproofing, Leather & Leatherette Covered Liners, One (1) Metal Finished Handle Electrically Operated Passenger Steps (LH and RH) with Boarding Lights (in lieu of fixed steps) Customized VIP Cabin Finishing Decoration Trim Passenger Carpet P.A. (Passenger Address) System (including loudspeakers and safety belts lights) ICS in the Cabin for All Passengers Passenger Cabin Thermo Acoustic Double Layer Tinted Windows Cabin Vertical Handles Alternate Current (AC) Power Outlet Coat Hooks 'FiveStar' Comfort Package Air Conditioning System AVCS Hydraulic Pulsation Dampeners MGB Premium Grade MVA Nose Landing Gear Doors An Important Note About Buying An Aircraft Aircraft Shopper Online takes internet fraud very seriously. Before completing any transaction, please review our fraud prevention guidelines to protect yourself. Read our Fraud Alert → Listed By Aero Asset Inc Location Toronto, CA Website Visit website Contact Information Contact: Emmanuel Dupuy Tel: (732) 578-8217 181 Bay Street Toronto, M5J 2T9Tor Canada More listings from Aero Asset Inc