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2025 LEONARDO AW189

Preis auf Anfrage
None
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KI-Preisbewertung (gem. EU AI Act, Art. 13): Diese Preisbewertung ist eine automatisierte, nicht-verbindliche Schätzung auf Basis vergleichbarer Marktdaten — sie stellt weder eine Kaufpreisempfehlung noch eine gutachterliche Wertermittlung dar. Für eine verbindliche Bewertung empfehlen wir, einen anerkannten Luftfahrt-Sachverständigen hinzuzuziehen.

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

Baujahr
2025
Standort
New York, New York, USA
Quelle
controlleremea.co.uk
Online seit
2026-08-27 🟢 Neu
Daten täglich aktualisiert
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