2025 Agusta AW109 Trekker for sale

2025 Agusta AW109 Trekker

Twin Turbine Helicopter

FOR SALE
Contact for price
Location Panama, Panama
Seats 8
Engine Rolls Royce M250
Cruise 148 kts (274 km/h)
ICAO Type A109
✓ Clean NTSB ✓ Verified recently

Aircraft Details

Seller reported

Avionics & Equipment

IFR
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.

Description

2025 AW109T Utility available for sale!

Engine

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

Propeller

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

Interior

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

Exterior

EXTERIOR FINISHING Finishing accordance with manufacturer specification Primer exterior painting

Modifications / STCs

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)

Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.

Price Comparison 1 active offer

Source Price Action
Synerjet
controller.com
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Synerjet
aviationtrader.com.au
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Contact for price
Synerjet
controlleremea.co.uk
Contact for price *
Contact for price

* Converted to USD at daily European Central Bank (ECB) exchange rates

Estimate Monthly Payment

Agusta AW109 Trekker loan calculator

AeroGurus

AeroGurus Data & Analysis

Independent data from FAA, NTSB, and market analysis

About This Agusta AW109 Trekker

This 2025 Agusta AW109 Trekker is a 8-seat twin turbine helicopter . There are currently 7 AW109 Trekker aircraft listed for sale .

The AW109 Trekker cruises at 148 kts (274 km/h) with a range of 370 nm (685 km) — ideal for short hops and local flights. Service ceiling of 15,120 ft allows operation above most weather.

Operating costs: Fuel burn is 50 GPH (189 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $275/hr in fuel alone.

NTSB records show 0 incidents for this airframe — a clean safety record.

Pre-Purchase Checklist

Safety record: 0 NTSB incidents
Budget $750 for pre-purchase inspection

Agusta AW109 Trekker — Model Specs

Model specification

Standard specs for this model. Actual aircraft may differ.

Seats
8
Cruise Speed
148 kts (274 km/h)
Range
370 nm (685 km)
Ceiling
15,120 ft (4,609 m)
Max Weight
7,000 lbs (3,175 kg)
Useful Load
2,181 lbs (989 kg)
Horsepower
1470 HP
Fuel Capacity
152 gal (575 L)
Fuel Burn
50 GPH (189 L/h)
Engines
2

Estimated Cost of Ownership

AeroGurus estimate

AGUSTA AW109 Trekker

Fuel Burn
50.0 GPH
~$325/hr

AeroGurus estimates based on industry averages for the AGUSTA AW109 Trekker. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.

Ownership & Registration

Registration number not available.

Location & Ownership

FAA records

Aircraft Location

Panama, Panama

PA

Seller reported

Title Status

No FAA title records

Available for US-registered aircraft only

Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.

Safety Record

NTSB safety data coming soon.

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Prices and listings updated daily · Data: FAA Registry, NTSB · About our data
Disclaimer: All prices, cost estimates, and market values shown are based on asking prices from third-party sources and are provided for informational purposes only. AeroGurus is not an appraiser, broker, or financial advisor. Always obtain a professional appraisal and independent inspection before making a purchase decision. Actual transaction prices may differ from asking prices.