2025 LEONARDO AW189
Preis auf Anfrage
Standort des Flugzeugs:New York, New York, USA
Verkäuferinformation
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Beschreibung
Spezifikation
Jahr2025
HerstellerLEONARDO
ModellAW189
SeriennummerL-1309
ZustandNeu
FlugregelnIFR
Flugzeit0
ZusatztreibstofftankJa
Absturzsicheres KraftstoffsystemJa
Altimetrisches RadarJa
ELTJa
BordwetterradarJa
Verkehrswarn- und KollisionsvermeidungssystemJa
Avionik/FunkgeräteADELT 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
DoppelsteuerungJa
KlimaanlageJa
Zusätzliche AusrüstungAir 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
AusstattungOffshore
SchallisolierungJa