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2025 Agusta AW189Turbine Helicopter • New York, NY, USA

This factory-new 2025 Leonardo AW189 turbine helicopter, serial number L-1309, is offered in an OGP-compliant offshore configuration with zero total time on the airframe. It is powered by General Electric GE CT7-2E1 engines and carries a warranty valid until December 2028 or 2,000 hours. The aircraft is IFR-certified and equipped with a Goodrich hoist, soundproofing, high-visibility rotor blades, and an environmental control system with air conditioning. Floor provisions allow for a multiple-seat layout, and the aircraft includes auxiliary fuel tanks and a crash-resistant fuel system.

The avionics package is built around an enhanced...

Year
2025
Make
Agusta
Series
AW189
Model
AW189
Serial #
L-1309

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Specifications

Category
Turbine Helicopter
Intended Use
Passenger, Search and Rescue, Utility
Flight Rules
IFR

Hours, Logs & Inspections

Avionics

GPS

GPS - 2nd GPS; ADELT with GPS NAV interface and GPS integrated

Comms

HF 9031 - Radio HF Provision; Radio VHF/FM-H Maritime NAT NPX (FP+RP); Digital Map

Weather

Telephonics RDR-1600 - Airborne Weather Radar; Weather Radar (FP+RP)

Traffic

Rockwell Collins TCAS II - TCAS II integrated with ATC Transponder Mode with ADS-B out capability

ADSB

Mode S Transponder - ATC with ADS-B out capability

Additional Equipment

Radar Altimeter

2nd Radar Altimeter

ELT

ADELT - ADELT with GPS NAV interface and GPS integrated in lieu of standard ELT

Enhanced Offshore Avionic Package

Offshore FMS - FMS Automatic Oil Rig Approach; HTAWS Mode; Helicopter Data Transmission (FP)

Health and Usage Monitoring System

HUMS - Health and Usage Monitoring System (HUMS); Flight Data Monitoring (FDM)

Helicopter Terrain Avoidance & Warning System

HTAWS - Helicopter Terrain Avoidance Warning System (HTAWS)

RNP Approach

RNP Approach with LPV/LP minima; RNP 0.3 navigation in all phase of flight; FMS capability

SATCOM

Flightcell DZMx - with integrated Wifi module (FP+RP)

Flight Recorder

EAFR - One solid state Cockpit and Voice Enhanced Airborne Flight Recorder (EAFR) with provision for video recording capability and ULB; Camera in the Cockpit (EAFR)

Rescue Hoist

Goodrich - Rescue hoist Dual type Provision; Swivelling Light for Rescue Hoist (belly mounted) Provision

Air Conditioning

ECS - Environmental Control System (ECS) Air Conditioning

Dual Controls

Emergency Floats and Life Rafts

Integrated Emergency Floats and Life Rafts (2x21) – (FP+RP); Life Rafts 3rd Handle

Helicopter Emergency Exit Light System

HEELS - Helicopter Emergency Exit Light System (HEELS); Electrical Emergency Exit Markings

Strobe Lights

Strobe Lights on the Winglets – In lieu of 2nd Anti-Collision Light; High Intensity Strobe Light

Auxiliary Fuel Tank

Two (2) “Under Floor” fuel tanks (190 kg – 419lb/238 l – 63 US Gallons) – Removable

Crash-Resistant Fuel System

Refuelling System

Filler port for controlled pressure refuelling/defuelling system (RH) & second filler port for gravity refuelling

Rotor Brake System

Main rotor hub Beanie; Rotor Brake System; Provision for main rotor Blade Tracking (magnetic pick-up)

Soundproofing

Soundproofing; Offshore Soundproofing

High Visibility Rotor Blades

High Visibility Rotor Blades Painting

Power Generation System

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); 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

Harsh Maritime Environments Protection

Maritime Protection Altitude Extension

Maritime Protection Altitude Extension 15,000 ft

Fire Extinguishers

Two fire Extinguishers (cockpit and cabin – EU OPS 3 compliant)

First Aid Kit

First aid Kit (EU OPS 3 compliant)

Baggage Compartment

Carpet on the baggage compartment Floor; Baggage compartment utility finishing Interior (carbon-fibre and soft liner); Baggage smoke Sensor; Baggage Compartment Net; Protection for baggage compartment Edge; Baggage compartment net provision

Cabin Separation Wall

Cockpit Cabin separation Wall (soft type)

Passive Vibration Absorbers

Two cockpit Passive Vibration Absorbers

Camera

Camera on the Tail Fin

Sun Shades

Two cockpit panel sun-glare Shields; Overhead cockpit windows sun Shades

Maintenance Step

Maintenance Step (RH side)

Cockpit and Cabin Access Steps

Two steps for cockpit and cabin access (on both fuselage side)

Seats

Pilot and Co-pilot crashworthy adjustable Seats (with inertial reels and separate 5 points safety belts)

Headsets

Pilot and Co-pilot Headsets; Pilot and Co-pilot headset Hooks (overhead)

Power Outlet

28V DC cockpit/cabin power Outlet (interseat console); Interseat console extension with multipurpose pocket (if compatible with console panels layout)

Documentation

Rotorcraft Flight Manual and Quick Reference Handbook; Two portable Flashlights (Cockpit)

Protection

Nose Landing Gear bay Protection

Back-up Battery

ISIS - Back-up battery for ISIS

Interior & Exterior

Interior Notes
HD Interior Configuration; Offshore Soundproofing
Exterior Notes
High Visibility Rotor Blades Painting

Engine & Propeller

Engine Type
Turboshaft
Engine Count
2
Engine Make
General Electric
Engine Model
GE CT7-2E1

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Aircraft Location

New York, NY, USA

Listing Details

New
For Sale

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First Seen: Aug 7, 2026

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