2024 Agusta AW109 TREKKER for sale, England, United Kingdom

Dual Pilot IFR package (in addition to Single Pilot VFR STD configuration)
-Dual controls
-Co-Pilot large colour Primary Flight Display (PFD) embedding:
▪Synthetic Vision System (SVS)
▪Highway In The Sky (HITS)
▪Helicopter Terrain Awareness and Warning System (HTAWS)
▪Flight Management System (FMS)
▪Radio tuning controls
2nd VHF/AM
2nd VOR/ILS
2nd GPS
DME
Marker beacon
Electronic Standby Indicator
Co-Pilot Intercommunication System (ICS)
Dual Master warning lights
Dual Master caution lights
2nd Magnetic Compass indicator
Digital clock
Flight Director
4-axis AFCS in lieu of 3-axis duplex SP-711 Honeywell
Emergency Locator Transmitter
Traffic Advisory System TAS-620 Avydine Or equivalent model

Executive interior - 6 places
VIP Passenger Cabin, including:
▪Soundproofing
▪Liners leather or leatherette covered
▪Cabin loudspeakers (Qty. 2)
▪Reading lights, advisory lights, floor courtesy lights
▪Upper and lower air vents
▪VIP Cabin finishing
VIP Cockpit package, including:
▪Interseat console tray with 12 V power supply
▪Multipurpose holder (with space provision for fire extinguisher)
▪Door pockets (RH and LH)
▪Headset hooks (Qty 2)
▪Cyclic and collective leather gators
▪Curtains in cockpit on upper windows
▪VIP Cockpit finishing
Three (3) crashworthy fwd facing seats (aft bench) covered with leather, with
foldable armrest
Three (3) crashworthy aft facing seats (central bench) covered with leather, with
see-through modification and with foldable armrest
4-point shoulder harness with inertial reels and safety belts for all passenger
seats
Cabin double layer acrylic windows (azure coloured)
Headset Bose ANR type (Qty 6)
Floor carpeting
Coat hooks in passengers cabin (Qty. 4)
Single central drawer Under central bench
USB charger at central bench (LH)

Interior Arrangement
H10-13H David Clark headsets (pilot and co-pilot)
Crash-resistant pilot seat, fore and aft adjustable, with lap belts and headrest
Shoulder harness with inertial reels (pilot)
Aluminium alloy honeycomb reinforced floor with anti-skid finishing
Ventilation ram air inlets
Anti-reflection instrument panel
Primer finished cabin walls
Portable fire extinguisher

White with black tail boom

Transmission / Drive System and Hydraulic System
960 shp for take-off and 900 shp continuous operation main transmission
3-stage transmission
Two (2) free wheeling units
Dual independent, redundant hydraulic systems
Two (2) transmission mounted hydraulic pumps with separate reservoir
Internal dry sump transmission lubrication with pressure and scavenge pump and oil
filter
Two (2) transmission oil chip detectors
Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip
detector
Transmission cooling and lubrication system
Transmission shafts

Electrical System
24 V DC 33 Ah nickel-cadmium battery with temperature probe
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)
External power receptacle
Position lights (NVG friendly - green, red, white)
Taxing light (one [1] RH) and landing light (one [1] LH)
Two (2) anti-collision lights (NVG friendly)
Two (2) cockpit utility lights
Instrument lights with dimming switch
Radio master switch with ground function

Single Pilot VFR Avionic Package
Two 6” x 8” display units providing a Primary Flight Display (PFD) and a Multifunction
Display (MFD) and integrating:
– Synthetic Vision System (SVS)
– Highway In The Sky (HITS)
– Helicopter Terrain Awareness and Warning System (HTAWS)
– Flight Management System (FMS)
– Radio tuning controls
Dual Data Acquisition Unit (DAU)
Dual Air Data Computer and Attitude Heading Reference System (ADAHRS)
VHF/AM
VOR/ILS
GPS
Mode-S & ADS-B Out Transponder
Pilot Intercommunication System (ICS)
Magnetic Direction indicator

Systems Data (on displays)
Dual Inter turbine gas temperature indicator (ITT°C)
Dual Engine torque indicator (TQ%)
Dual Compressor speed indicator (N1%)
Dual Turbine speed indicator (N2%)
Rotor speed indicator (NR%)
Dual Transmission oil pressure (PSI) and temperature (°C) indicator
Dual Engine oil pressure (PSI) and temperature (°C) indicator
Dual Fuel pressure (PSI) and fuel quantity (kg) indicator
Dual hydraulic pressure system indicators (PSI)
Outside air temperature indicator (°C)
Dual DC voltmeter (VDC)
Dual DC ammeter (Amp)

Warning/Caution Advisory and Maintenance System
Master warning lights
Master caution lights
Warning, caution and advisory messages
Aural alerts
Engines fire detection system

Premium Equipment
Crash-resistant co-pilot seat, fore and aft adjustable, with lap belts and headrest
Shoulder harness with inertial reels (co-pilot)
AC power supply system (two [2] inverters)
AFCS 3-axis duplex SP-711 Honeywell
Radar altimeter
Doors key lock
Airframe hourmeter
Baggage compartment lights
Crew open door actuators
Two (2) engine compartment fire extinguishers
Fuel cap with key-lock
Pulsed chip detector In lieu of quick disconnecting chip detectors.
450 W Retractable/rotating landing light Nose mounted.
Reinforced windshield
Baggage compartment extension (1.9 m)
Bleed air heater
Passenger foot step (RH)

Miscellaneous / Ground Equipment
Air intake/exhaust covers
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)