2021 AgustaWestland AW109 Trekker

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Description

The AgustaWestland AW109 Trekker is a light-twin utility helicopter manufactured by AgustaWestland. The Trekker was designed to fill the role of a light utility helicopter. It is powered by two Pratt & Whitney Canada PT6C-67C engines, and is equipped with a single main rotor and tail rotor system. The Trekker has been used by various military, law enforcement and civilian customers around the world. It is capable of performing various missions such as search and rescue, personnel transport, cargo transport, and aerial surveillance. The AW109 Trekker is a reliable, versatile and cost-effective solution for a wide range of missions.

Features

  • Total Time: 92
  • ENGINES:
  • Model: Two Pratt & Whitney Canada PW207C
  • Engine #1
  • TTSN 91.6 hours
  • TCSN 162 cycles
  • Engine #2
  • TTSN 91.6 hours
  • TCSN 162 cycles
  • AVIONICS:
  • 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
  • Emergency Locator transmitter
  • Enhanced vision system (EVS) EVS-23000 Max-Viz (Removable part will be provided in retrofit after delivery, at the end of the certification activity)
  • Digital map Euronav VII Euroavionics (The standard global package includes: Raster map data: Euroavionics outline map (basic detail), Euroavioncs Map 1:1.000.000, Vector map data: Euroavionics Overview map (basic detail), Terrain data: DTED 0, Database: Jeppensen NavData, Additional maps/options and any updates need to be ordered directly to Euroavionics by the customer)
  • Traffic Advisory System TAS-620 Avydine (Or equivalent model)
  • Weather radar RDR 2000 Bendix/King (Or equivalent model)
  • OPTIONAL 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 hour meter
  • Baggage compartment lights
  • Crew open door actuators
  • Two (2) engine compartment fire extinguishers
  • Fuel cap with key-lock
  • Pulsed chip detectors (In 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 foot step (RH)
  • Air conditioning ECU
  • Dual USB charger at central bench (RH)
  • Mast Vibration Absorver (MVA)
  • Cockpit access handle (RH)
  • Cockpit access handle (LH)
  • First aid kit
  • Baggage compartment extension (2.3 m)
  • Vertical baggage compartment door (in lieu of standard type)
  • Rotor brake
  • Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
  • 213 USgal crash-resistant fuel system (in lieu of 152 USgal)
  • Strobe lights on horizontal stabilizer
  • Long step bar (LH)
  • Long step bar (RH) (in lieu of standard passenger foot step (RH)
  • MISCELLANEOUS / GROUND EQUIPMENT:
  • Air intake/exhaust covers
  • Ground tools kit (including tow bar, ground wheels, lifting tool)
  • Pilot tubes covers
  • Rotorcraft Flight Manual (RFM) (hard copy) and technical publications (soft copy)
  • Tie-down fittings (main rotor retention straps)

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