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Helicopter

2025 LEONARDO AW189

🕒 Listed 2 months ago
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fyiEstimate $858,500–$880,500 ⓘ How this estimate is built

Starts from the median asking price of 165 comparable Helicopter listings ($760,000), then adjusts for:

  • Year +1 vs comparable listings +1.5%
  • ADS-B (36% of comps) +12.7%

Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.

2025
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L-1309
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★ 4.2 (5 Google reviews)

Overview

Make / ModelLeonardo AW189
TypeHelicopter
Airframe time—
Avionics / Weather radarRDR-1600
Avionics / Traffic (TCAS / TAS)TCAS II
ADS-B

Description

FACTORY NEW OFFSHORE AW189 OGP Compliant Offshore Layout Hoist - Goodrich (FP) Soundproofing Floor provisions for multiple-seats layout Configuration Environmental Control System (ECS) - Air Conditioning High Visibility Rotor Blades Painting Warranty until 12/28 or 2,000hrs General Electric GE CT7-2E1 Engines We offer the Aircraft : “As-is”, Ex-Works North America

Modifications

Air Conditioning System Carpet on the baggage compartment Floor Camera in the Cockpit (EAFR) Integrated Emergency Floats and Life Rafts (2×21) – (FP+RP) Life Rafts 3rd Handle Helicopter Emergency Exit Light System (HEELS) Strobe Lights on the Winglets – In lieu of 2nd Anti-Collision Light Filler port for controlled pressure refuelling/defuelling system (RH) & second filler port for gravity refuelling Harsh Maritime Environments Protection Swivelling Light for Rescue Hoist (belly mounted) – Provision High Intensity Strobe Light Cockpit Cabin separation Wall (soft type) Electrical Emergency Exit Markings ELA and life jackets removals Cockpit tinted upper Window DC / AC primary power generation system: 28 V DC / 115 V AC 400 Hz provided by three independent 25kVA Starter Generators (one for each engine and for APU) Two Starter Generator Converter Units One Generator Control Unit (GCU) for APU Three Transformer Rectifier Units (TRU) Rescue hoist (Goodrich) – Dual type – Provision – DELTA PRICE In lieu of the kit “Rescue hoist (Goodrich) – Single type – Provision” One battery (17 Ah) 28 V DC External Power Receptacle 115 V AC External Power Receptacle DC Power Distribution System & AC Power Distribution System Solid-State Secondary DC Power Distribution System Display based Virtual Circuit Breaker Panel Reduced Overhead Circuit Breaker Panel Cockpit compartment utility finishing Interior Two cockpit panel sun-glare Shields Pilot and Co-pilot crashworthy adjustable Seats (with inertial reels and separate 5 points safety belts) Pilot and Co-pilot Headsets 28V DC cockpit/cabin power Outlet (interseat console) Interseat console extension with multipurpose pocket (if compatible with console panels layout) Baggage compartment utility finishing Interior (carbon-fibre and soft liner) Baggage smoke Sensor Baggage Compartment Net Two (2) “Under Floor” fuel tanks (190 kg – 419lb/238 l – 63 US Gallons) – Removable Two steps for cockpit and cabin access (on both fuselage side) Main rotor hub Beanie Rotor Brake System Provision for main rotor Blade Tracking (magnetic pick-up) 2nd anti-collision Light Overhead cockpit windows sun Shades First aid Kit (EU OPS 3 compliant) Two fire Extinguishers (cockpit and cabin – EU OPS 3 compliant) Pilot and Co-pilot headset Hooks (overhead) Rotorcraft Flight Manual and Quick Reference Handbook Two portable Flashlights (Cockpit) Nose Landing Gear bay Protection Protection for baggage compartment Edge Baggage compartment net provision Back-up battery for ISIS Maintenance Step (RH side) Two cockpit Passive Vibration Absorbers Camera on the Tail Fin Maritime Protection Altitude Extension 15,000 ft HD

Avionics

ADELT with GPS NAV interface and GPS integrated In lieu of standard ELT Digital Map Radio HF 9031 – Provision Radio VHF/FM-H Maritime NAT NPX 138 – (FP+RP) Weather Radar Telephonics RDR-1600 – (FP+RP) SATCOM Flightcell DZMx with integrated Wifi module (FP+RP) 2nd radar Altimeter 2nd GPS One solid state Cockpit and Voice Enhanced Airborne Flight Recorder (EAFR) with provision for video recording capability and ULB Enhanced Offshore Avionic Package: Offshore FMS Automatic Oil Rig Approach; HTAWS Offshore Mode; Helicopter Data Transmission (FP) TCAS II (Rockwell Collins) integrated with ATC Transponder Mode S with ADS-B out capability Health and Usage Monitoring System (HUMS) Flight Data Monitoring (FDM) Helicopter Terrain Avoidance & Warning System (HTAWS) RNP Approach with LPV/LP minima “RNP 0.3 navigation in all phase of flight” FMS capability

Recommended avionics upgrades

Garmin GTN 650Xi

No IFR GPS navigator is listed — a GTN 650Xi is the standard entry point for WAAS/LPV capability.

See prices & suppliers ›
Garmin GFC 500 autopilot

No autopilot is listed — a GFC 500 (or S-TEC 3100 / Trio Pro Pilot where the GFC isn't STC'd) adds a modern digital autopilot with envelope protection, subject to model approval.

See prices & suppliers ›

Suggestions are based on the panel described in this listing; verify STC approval for this make/model before any installation.

Service Difficulty Reports (SDRs)

Checking FAA service difficulty reports…

Airworthiness Directives (ADs)

Checking airworthiness directives…

General

Year2025
ManufacturerLEONARDO
ModelAW189
Serial NumberL-1309
ConditionNew
FlightRulesIFR

Airframe

Total Time0
Auxiliary Fuel TankYes
Crash-Resistant Fuel SystemYes

Avionics

Radar AltimeterYes
ELTYes
Airborne Weather RadarYes
Traffic Avoidance SystemYes
Avionics/RadiosADELT with GPS NAV interface and GPS integrated In lieu of standard ELT Digital Map Radio HF 9031 – Provision Radio VHF/FM-H Maritime NAT NPX 138 – (FP+RP) Weather Radar Telephonics RDR-1600 – (FP+RP) SATCOM Flightcell DZMx with integrated Wifi module (FP+RP) 2nd radar Altimeter 2nd GPS One solid state Cockpit and Voice Enhanced Airborne Flight Recorder (EAFR) with provision for video recording capability and ULB Enhanced Offshore Avionic Package: Offshore FMS Automatic Oil Rig Approach; HTAWS Offshore Mode; Helicopter Data Transmission (FP) TCAS II (Rockwell Collins) integrated with ATC Transponder Mode S with ADS-B out capability Health and Usage Monitoring System (HUMS) Flight Data Monitoring (FDM) Helicopter Terrain Avoidance & Warning System (HTAWS) RNP Approach with LPV/LP minima “RNP 0.3 navigation in all phase of flight” FMS capability

Additional Equipment

Dual ControlsYes
A/CYes
Additional EquipmentAir Conditioning System Carpet on the baggage compartment Floor Camera in the Cockpit (EAFR) Integrated Emergency Floats and Life Rafts (2×21) – (FP+RP) Life Rafts 3rd Handle Helicopter Emergency Exit Light System (HEELS) Strobe Lights on the Winglets – In lieu of 2nd Anti-Collision Light Filler port for controlled pressure refuelling/defuelling system (RH) & second filler port for gravity refuelling Harsh Maritime Environments Protection Swivelling Light for Rescue Hoist (belly mounted) – Provision High Intensity Strobe Light Cockpit Cabin separation Wall (soft type) Electrical Emergency Exit Markings ELA and life jackets removals Cockpit tinted upper Window DC / AC primary power generation system: 28 V DC / 115 V AC 400 Hz provided by three independent 25kVA Starter Generators (one for each engine and for APU) Two Starter Generator Converter Units One Generator Control Unit (GCU) for APU Three Transformer Rectifier Units (TRU) Rescue hoist (Goodrich) – Dual type – Provision – DELTA PRICE In lieu of the kit “Rescue hoist (Goodrich) – Single type – Provision” One battery (17 Ah) 28 V DC External Power Receptacle 115 V AC External Power Receptacle DC Power Distribution System & AC Power Distribution System Solid-State Secondary DC Power Distribution System Display based Virtual Circuit Breaker Panel Reduced Overhead Circuit Breaker Panel Cockpit compartment utility finishing Interior Two cockpit panel sun-glare Shields Pilot and Co-pilot crashworthy adjustable Seats (with inertial reels and separate 5 points safety belts) Pilot and Co-pilot Headsets 28V DC cockpit/cabin power Outlet (interseat console) Interseat console extension with multipurpose pocket (if compatible with console panels layout) Baggage compartment utility finishing Interior (carbon-fibre and soft liner) Baggage smoke Sensor Baggage Compartment Net Two (2) “Under Floor” fuel tanks (190 kg – 419lb/238 l – 63 US Gallons) – Removable Two steps for cockpit and cabin access (on both fuselage side) Main rotor hub Beanie Rotor Brake System Provision for main rotor Blade Tracking (magnetic pick-up) 2nd anti-collision Light Overhead cockpit windows sun Shades First aid Kit (EU OPS 3 compliant) Two fire Extinguishers (cockpit and cabin – EU OPS 3 compliant) Pilot and Co-pilot headset Hooks (overhead) Rotorcraft Flight Manual and Quick Reference Handbook Two portable Flashlights (Cockpit) Nose Landing Gear bay Protection Protection for baggage compartment Edge Baggage compartment net provision Back-up battery for ISIS Maintenance Step (RH side) Two cockpit Passive Vibration Absorbers Camera on the Tail Fin Maritime Protection Altitude Extension 15,000 ft HD

Interior

ConfigurationOffshore
SoundproofingYes

Range from base

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