2025 Agusta Leonardo AW109 Trekker

General

Manufacturer

LEONARDO

Model

AW109 TREKKER

Condition

Used

Airframe

Total time

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

Avionics

• 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

• 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

• 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.

Equipment

• 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

• 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

• 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)

• 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)

• 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)

• Engines Inlet Barrier Filters (IBF)

Interior

Year Interior

2025

• 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

• 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

Exterior

Year Painted

2025

• Finishing accordance with manufacturer specification
• Primer exterior painting