A brand new helicopter currently under manufacture, scheduled for delivery in January 2026.
General Descriptions:
Total Time: Delivery Hours
No. of Crew & Pax: 2 Crew & 12 Pax
MTOW: 7 000 kg / 15 432 lbs
manufacturer
Leonardo
model
AW139
configuration
Offshore
condition
New
year
2026
time
0
helicopter location
Italy
serial number
TBA
registration number
TBA
listing ID
HT24331
Description
avionics
7 Phase Avionics
Honeywell Primus Epic Phase 7 Avionic System
Pilot and Co-pilot Primary Flight Display (PFD)
External Dimensions: 8" × 10". Color Active-Matrix Liquid Crystal Display (AMLCD)
Pilot and Co-pilot Multi-Function Display (MFD)
External Dimensions: 8" × 10". Color Active-Matrix Liquid Crystal Display (AMLCD)
Electronic Standby Instrument System (ESIS)
Displaying Attitude, Airspeed, Altitude, Vertical Speed, Compass and ILS Data
2x Attitude and Heading Reference Systems (AHRS)
2x Air Data Modules (ADM)
2x Flux Valves
2x Display Controllers
2x Cursor Control Devices (CCD)
Reversion Control Panel (RCP)
Display Dimming Control Panel (DCP)
Stability Augmentation System (SAS) Control Panel
2x Remote Instrument Controllers (RIC)
2x Pedestal Mounted Multifunction Control Display Units (MCDU)
2x Modular Avionic Units (MAU), including the following major subsystems and/or functions:
Dual Vehicle Monitoring System (VMS)
Dual Monitor Warning System (MWS)
Single Aural Warning Generator (AWG)
Single Central Maintenance Computer (CMC)
Provision for (CVR/FDR) Data Interface
Pilot and Co-Pilot Interphone Control
Cyclic Grip and Floor Switches
Left Modular Radio Cabinet (MRC), including:
VHF Radio
VOR/LOC/GS/MB
Right MRC, including:
VHF Radio
VOR/LOC/GS/MB
Automatic Direction Finder (ADF)
Distance Measuring Equipment (DME)
Flight Guidance Controller
Pilot and Co-Pilot Digital Audio Panels
Including Remote ICS Audio Plug for Ground Operations
Pilot and Co-pilot Digital Clock
Magnetic Compass
Outside Air Temperature (OAT) Indicator
2x Master Warning Lights (MWL)
2x Master Caution Lights (MCL)
Engine 1 & 2 Fire Light
Baggage Compartment Smoke Detector Light
Dual Electrical Power Connection for CVR/FDR
Compliant to the Federal Aviation Administration (FAA) Requirement
Honeywell Primus Epic Phase 7 Avionic System
Pilot and Co-pilot Primary Flight Display (PFD)
External Dimensions: 8" × 10". Color Active-Matrix Liquid Crystal Display (AMLCD)
Pilot and Co-pilot Multi-Function Display (MFD)
External Dimensions: 8" × 10". Color Active-Matrix Liquid Crystal Display (AMLCD)
Electronic Standby Instrument System (ESIS)
Displaying Attitude, Airspeed, Altitude, Vertical Speed, Compass and ILS Data
2x Attitude and Heading Reference Systems (AHRS)
2x Air Data Modules (ADM)
2x Flux Valves
2x Display Controllers
2x Cursor Control Devices (CCD)
Reversion Control Panel (RCP)
Display Dimming Control Panel (DCP)
Stability Augmentation System (SAS) Control Panel
2x Remote Instrument Controllers (RIC)
2x Pedestal Mounted Multifunction Control Display Units (MCDU)
2x Modular Avionic Units (MAU), including the following major subsystems and/or functions:
Dual Vehicle Monitoring System (VMS)
Dual Monitor Warning System (MWS)
Single Aural Warning Generator (AWG)
Single Central Maintenance Computer (CMC)
Provision for (CVR/FDR) Data Interface
Pilot and Co-Pilot Interphone Control
Cyclic Grip and Floor Switches
Left Modular Radio Cabinet (MRC), including:
VHF Radio
VOR/LOC/GS/MB
Right MRC, including:
VHF Radio
VOR/LOC/GS/MB
Automatic Direction Finder (ADF)
Distance Measuring Equipment (DME)
Flight Guidance Controller
Pilot and Co-Pilot Digital Audio Panels
Including Remote ICS Audio Plug for Ground Operations
Pilot and Co-pilot Digital Clock
Magnetic Compass
Outside Air Temperature (OAT) Indicator
2x Master Warning Lights (MWL)
2x Master Caution Lights (MCL)
Engine 1 & 2 Fire Light
Baggage Compartment Smoke Detector Light
Dual Electrical Power Connection for CVR/FDR
Compliant to the Federal Aviation Administration (FAA) Requirement
equipment
Aluminum Alloy and Composite Fuselage
Acrylic Windshields
Overhead Cockpit
Transparent Windows
Lower Cockpit
Transparent Windows
Pilot and Co-Pilot Lower Door Windows
Cockpit Ram Air Adjustable Outlets
Heated Pitot Tube (Qty. 2) with Pitot Heat Failure Warning (Qty. 2)
Heated Static Intake (Qty. 2)
Cockpit Fire Extinguisher
Cabin Fire Extinguisher
Plug-In Sliding Door (Qty. 2) for Passenger Cabin Access with Locking Latch (Qty. 4) and Additional Sliding Doors Cabin Handle (Qty. 2, one on each side)
Pilot Door (Qty. 2) with Push-Out Emergency Exit Window
Including Storm Window on Pilot's Side
Passenger Doors Stop in Fully Open Position
Cabin Push-Out Emergency Exit Window (Qty. 6)
Two (2) of which installed on Each Passenger Cabin Door
Baggage Compartment with Lockable Baggage Compartment Door (Qty. 2, LH and RH)
Wheeled Retractable Tricycle Landing Gear
Comprising Two (2) Wheels on Nose Landing Gear and Brakes on Main Landing Gear
Structural Provisions for Nose Landing Gear Doors
Landing Gear Mooring
Provisions for Upper Deck Mooring
Hoisting and Jacking Fittings
Tail Boom and Vertical Fin
Horizontal Stabilizer with Composite “Winglets”
Pilot and Co-Pilot Windshield Wipers
Maintenance Steps
Granting Upper Deck Accessibility on Both Sides
Upper Deck Cowlings
One (1) Front Forward Sliding, Two (2) Side Opening for Engine Access
Cockpit Footsteps
Cabin Footsteps
Utility Adaptive Anti Vibration Control System (AVCS) with Rotary Damping Masses
Acrylic Windshields
Overhead Cockpit
Transparent Windows
Lower Cockpit
Transparent Windows
Pilot and Co-Pilot Lower Door Windows
Cockpit Ram Air Adjustable Outlets
Heated Pitot Tube (Qty. 2) with Pitot Heat Failure Warning (Qty. 2)
Heated Static Intake (Qty. 2)
Cockpit Fire Extinguisher
Cabin Fire Extinguisher
Plug-In Sliding Door (Qty. 2) for Passenger Cabin Access with Locking Latch (Qty. 4) and Additional Sliding Doors Cabin Handle (Qty. 2, one on each side)
Pilot Door (Qty. 2) with Push-Out Emergency Exit Window
Including Storm Window on Pilot's Side
Passenger Doors Stop in Fully Open Position
Cabin Push-Out Emergency Exit Window (Qty. 6)
Two (2) of which installed on Each Passenger Cabin Door
Baggage Compartment with Lockable Baggage Compartment Door (Qty. 2, LH and RH)
Wheeled Retractable Tricycle Landing Gear
Comprising Two (2) Wheels on Nose Landing Gear and Brakes on Main Landing Gear
Structural Provisions for Nose Landing Gear Doors
Landing Gear Mooring
Provisions for Upper Deck Mooring
Hoisting and Jacking Fittings
Tail Boom and Vertical Fin
Horizontal Stabilizer with Composite “Winglets”
Pilot and Co-Pilot Windshield Wipers
Maintenance Steps
Granting Upper Deck Accessibility on Both Sides
Upper Deck Cowlings
One (1) Front Forward Sliding, Two (2) Side Opening for Engine Access
Cockpit Footsteps
Cabin Footsteps
Utility Adaptive Anti Vibration Control System (AVCS) with Rotary Damping Masses
interior
Pilot and Co-pilot Adjustable Seat (with Inertia-Reel and Safety Belts)
Cockpit Dome/Storm Light
2x Cockpit Utility Lights
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
Pilot and Co-Pilot Flash Lights
Cabin ICS Panel with Plug for One Headset
First Aid Kit
Cockpit Dome/Storm Light
2x Cockpit Utility Lights
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
Pilot and Co-Pilot Flash Lights
Cabin ICS Panel with Plug for One Headset
First Aid Kit
exterior
Painting and Finishing – Standard
Maritime Protection
Maritime Protection
engine 1
Pratt & Whitney Canada PT6C-67C Turbo-Shaft Engines
Independent FADEC Systems with Auto-Start and Engine Control Functions for Normal, Emergency and Training Operations
Magnetic Chip Detectors
Integrated and Independent Engine Oil Coolers
Engine Firewall Protection (1x for each engine)
Fire Detection System
Fire Extinguisher System
Steel Engine Exhaust and Ejector (1x for each engine)
Independent Crashworthy Fuel Cells
Engine Supply Pumps
Submerged Fuel Tank Booster Pumps
Fuel Filter Assemblies
Engine Backup Controls
Mechanical and Electrical
Engine Manual Start and Ignition Systems
Independent FADEC Systems with Auto-Start and Engine Control Functions for Normal, Emergency and Training Operations
Magnetic Chip Detectors
Integrated and Independent Engine Oil Coolers
Engine Firewall Protection (1x for each engine)
Fire Detection System
Fire Extinguisher System
Steel Engine Exhaust and Ejector (1x for each engine)
Independent Crashworthy Fuel Cells
Engine Supply Pumps
Submerged Fuel Tank Booster Pumps
Fuel Filter Assemblies
Engine Backup Controls
Mechanical and Electrical
Engine Manual Start and Ignition Systems
engine 2
Pratt & Whitney Canada PT6C-67C Turbo-Shaft Engines
Independent FADEC Systems with Auto-Start and Engine Control Functions for Normal, Emergency and Training Operations
Magnetic Chip Detectors
Integrated and Independent Engine Oil Coolers
Engine Firewall Protection (1x for each engine)
Fire Detection System
Fire Extinguisher System
Steel Engine Exhaust and Ejector (1x for each engine)
Independent Crashworthy Fuel Cells
Engine Supply Pumps
Submerged Fuel Tank Booster Pumps
Fuel Filter Assemblies
Engine Backup Controls
Mechanical and Electrical
Engine Manual Start and Ignition Systems
Independent FADEC Systems with Auto-Start and Engine Control Functions for Normal, Emergency and Training Operations
Magnetic Chip Detectors
Integrated and Independent Engine Oil Coolers
Engine Firewall Protection (1x for each engine)
Fire Detection System
Fire Extinguisher System
Steel Engine Exhaust and Ejector (1x for each engine)
Independent Crashworthy Fuel Cells
Engine Supply Pumps
Submerged Fuel Tank Booster Pumps
Fuel Filter Assemblies
Engine Backup Controls
Mechanical and Electrical
Engine Manual Start and Ignition Systems
damage history
No damages (brand new)
