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...
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
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
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New York, NY, USA
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New York, NY, USA
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