2025 LEONARDO AW109 TREKKER

2025

Used

2025 AW109T Utility available for sale!

0

Configuration Utility - SAR Certification EASA/FAA • Aluminum aloy and bonded panel fuselage • Semi-monocoque aluminum alloy tail boom • New reinforced skid type landing gear • Two (2) hinged jettisonable crew doors (LH and RH) • Two (2) sliding passenger doors (LH and RH), 1,40m opening, with jettisonable Windows • Acrylic transparent windshield and side Windows • Acrylic transparent overhead Windows • Quick-removable tail rotor drive shaft cover • Separate baggage compartment with hinged door • Removable fairing and cowlings, for complete • Accessibility to he controls and drive components • Quick-opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points • Grounding points • Jacking and hosting points

ROTORS AND CONTROLS • Titanium mainrotor hub, corrosion protected, fully articulated with four (4) composite grips, four (4) elastomeric bearings, four (4) individually interchangeable composite material blades, swept tips, and dampers • Cyclic and collective contros powered by two (2) hydraulic systems • Hydraulically powered anti-torquesystem • Adjustable friction devices on cyclic and collective system • Forcem trim and artificial feel system • Adjustable directional control pedals • Flapping and droop restraint mechanism

POWER PLANT AND FUEL SYSTEM • Two(2) Pratt & Whitney Canada PW207C turboshaft engines • Two (2) independente electronic control systems (FADEC) with normal emergency and training operation modes and auto-start • Two (2) engine-mounted fuel pump and filter assembly Two (2) engine-mounted • Oil ump and filter assembly • Two (2) engine-mounted fuel controls and governor • Lubrification and cooling system Two (2) engine oil chip detectors • Engine control panel Two (2) independente fuel systems with cross-feeding valve and control panel • 3-cell crash -resistant fuel system (5751-152 USgal) • Two (2) submerged fuel boost pumps Airframe mounted eaysaccessfuel filter • RH refuelling point • Ground fuel drains

DUAL PILOT VFR AVIONIC PACKAGE • Three (3) 6" x 8" display units providing two (2) • Primary Flight Display (PFD) and one (1) • Multifunction Display(MFD) and integrating: - Synthetic Vision System (SVS) - Highway In The Sky (HITS) - Helicopter Terrain Awareness and Warning System (HTAWS) - Flight Management - Radio tuning controls • Dual Data Acquisition unit (Dau) • Dual Air Data Computer and Attitude Heading • VHF/AM • GPS • Mode-S & Ads-B Out Transponder • Pilot and Co-Pilot Intercommunication System (ICS) • Two (2) Magnetic Direction Indicators • Dual Master Warning Lights • Dual Master Caution Electronic • Standby Indicator • Dual Controls AVIONICS EQUIPMENT • Dual Pilot IFR Package • 2nd VHF/AM • 2nd VOR/ILS • 2nd GPS DME • Marker Beacon • Digital clock • Emergency Locator Transmitter (ELT) • Digital map Euronav VII Euro avionics • The standard Global Package includes: • Raster Map Data: EUROAVIONICS Outline Map (basic detail), EUROAVIONICS Map 1:1.000.000 • Vector Map Data: EUROAVIONICS Overview Map (basic detail) • Terrain Data: DTED 0 • Database: Jeppesen NavData • Additional maps/options and any updates need to be ordered directly to Euro avionics by the Customer.

TRANSMISSION DRIVE SYSTEM AND HYDRAULIC SYSTEM • 960shp fortake-off and 900 shp continuous operation ain transmission • 3-stage transmission • Two (2) freewhelling units • Dual independente, redundant hydraulic systems • Two (2) transmission-mounted hydraulic pumps with separate reservoir Internal dry sump • Transmission lubrication with pressure and sacavenge pump and oil filter • Two (2) transmission oil chip detectors • Single stage, bevel gear tail rotor 90º gear box including oil level sight glass and chip detector • Transmission cooling and lubrification system • Transmission shafits • Instrument lights with dimming switch • Radio master switch with ground function ELECTRICAL SYSTEMS • 24VDC 33Ah Nickel-cadmium battery with temperature problem • Two (2) 200 A self-cooled starter generators • Two (2) voltage regulators • Battery relay • Two (2) interconnecting bus relays • External power relay • Distribution buses (one [1] battery, two, [2 essential, two [2] emergency, two [2] main, two [2] auxiliary) • Distribution buses (one [1] battery, two, [2 essential, two [2] emergency, two [2] main, two [2] auxiliary) • External power receptacle • External power receptacle Position lights (NVG friendly - green, red, White) • Position lights (NVGfriendly- green, red, White) • Two (2) cockpit utility lights PREMIUM EQUIPMENT • Crash-resistant co-pilot seat, foreand aft adjustable, with lab belts and headrest • Shoulder harness with inertial reels (co-pilot) • AC power supply sistem (two [2] inverters) 4-axis Digital AFCS, • Integrating Flight Director functionalities • Radar altimer • Doors key lock • Airframe hourmeter • Baggage compartment lights • Crew open door actuator • Two (2) engine compartment fire extinguisher • Fuel cap with key-lock • Pulsed chip detectors (iIn lieu of quick-disconnecting chip detectors.) • 450 W Retractable/rotating landing light (Nose-mounted) • Reinforced windshield • Baggage compartment extension (1.9m) • Bleed air heater • Passenger footstep (RH) MISCELLANEOUS/GROUND EQUIPMENT • Ground tools kit (including tow bar, ground wheels, lifting tool) • Pitot tubes covers • Rotorcraft Flight Manual (RFM) (hard copy) and technical publications (soft copy) • Tie-down fittings (main rotor retention straps) ADDITIONAL EQUIPMENT, NOT INSTALLED • Engines Inlet Barrier Filters (IBF) UTILITY EQUIPMENT • First aid kit • Rotor brake • Windshield wipers for pilot and co-pilot • Cargo hook (1250 kg) - Provision • External rescue hoist(272 kg/600 lb) (Breeze) – Provision • Requires Wireless ICS Polycon system. • Wireless Communication Polycon Next Generation • Required for Human External Cargo (HEC) operations • Wire Strike Protection System • Rape ling hooks (2 LH – 2 RH)

2025

EXTERIOR FINISHING Finishing accordance with manufacturer specification Primer exterior painting

2025

INTERIOR ARRANGEMENT • H10-13H David Clark headsets (pilot and co-pilot) • Crash-resistant pilot seat, fore and aft • Shoulder harness with inertial reels (pilot) • Aluminum alloy honeycomb reinforced floor with anti-skid finishing • Ventilation ram air inlets • Anti-reflection instrument panel • Primer finished cabin walls • Portable fire extinguisher PROPOSED CONFIGURATION • Utility interior (Rigid liners) • Passenger cabin • All seats crash-resistant covered with leatherette • Three (3) fwd facing seats (aft bench) • Three (3) aft facing seats (central bench) • 4-point shoulder harness with inertial reels and safety belts for all seats • Rigid liners • Intercommunication system for passengers • Cabin loudspeakers (Qty 2) • Reading lights, advisory lights Upper and lower air vents • Headset H10-13H David Clark (Qty 6) • Cockpit equipment • Standard cockpit interior