Agusta A109E Power

260 hours | manufactured in 2009

ASA Consulting

The most successful bi-turbine helicopter in its category.

Range: 512 NM

Maximum cruise speed: 155 ktas

Seats: 1 pilot + 7 passengers

Characteristics

Airframe
  • Total Time: 260 hs
  • 657 Landings
BASIC AIRCRAFT
  • Standard aircraft with passengers cabin sliding doors, equipped with P&W206C engines, as per “Annex A of Enclosure 1”.
  • Standard modifications for 3000 Kgs. Maximum Take Off Weight1 modifications.
STANDARD ADDITIONAL EQUIPMENT
  • Internal structural provisions for utility equipment (cargo hook, rescue hoist, search light, AFCS)
  • Crew open door actuators
  • Tail boom strake
  • Fuel drain electrical valves
  • Pilot/copilot headsets (2)
  • Cabin Fire Extinguisher
  • First aid kit
  • Pilot/copilot shoulder harness with inertial reel
  • Quick disconnecting chip detectors
  • Baggage compartment lights
IFR AVIONIC PACKAGE (KING SILVER CROWN LINE)
  • AC system (2 inverters)
  • Pilot navigation instruments including
  • LCD EADI & EHSI
  • Stand-by ADI
  • Gyrocompass C14 A Honeywell
  • Vertical gyro (N.1) 46060-11 Flightline system
  • Vertical gyro (N.2) VG 208 JET Electronics
  • AFCS 3 Axis Duplex SP 711 Honeywell
  • ADF KR 87 King
  • Transponder (Mode S) KT 70 King
  • VHF-COM/NAV KX 165 King (2)
  • ICS Pilot / Co-pilot AG-06-1U Agusta/Gemelli
  • DME KDM 706A King
  • Marker Beacon KMR 675 King 1
  • Not available on Turbomeca Arrius equipped helicopter
ADDITIONAL AUXILIARY EQUIPMENT
  • Airframe hour meter
  • Baggage compartment extensions (1.9 m)
  • VLE & VLO extension up to 140 KIAS
  • Dual control
  • Rotor brake
  • Retractable landing light
  • Windshield wipers (Pilot/Copilot) with wiper switch on cyclic grip
  • Engine compartment fire extinguishers
  • Radio master switch with ground function
ADDITIONAL AVIONIC EQUIPMENT
  • Copilot flight/navigation instruments including:
  • LCD EADI & EHSI
  • Barometric altimeter
  • Air speed indicator
  • Vertical speed indicator
  • Flight Director & autotrim FZ 702 Honeywell
  • Radio altimeter AA300 Honeywell
  • E.L.T. (three frequencies) C 406-2HM Artex
  • GPS interfaced with EFIS and B-RNAV function 2101 I/O Trimble
  • EFIS Pilot/Copilot on Command Switch
  • Moving Map KMD 550 Bendix/King
    PAINTING
    • Agusta colour scheme from Agusta paint selection solid colour series 300
    AIRFRAME
    • Aluminium alloy and bonded panel fuselage
    • Semimonocoque aluminium alloy tail boom
    • Two hinged jettisonable crew doors (LH & RH)
    • Two passenger sliding doors (LH & RH) with jettisonable window
    • Acrylic windshield and side windows
    • Acrylic overhead windows
    • Removable fibreglass tail rotor gearbox fairing
    • Quick removable tail rotor drive shaft cover
    • Three wheel retractable landing gear
    • Interchangeable landing gear tires
    • Separate baggage compartment with hinged door
    • Three jacking points
    • Removable fairing and cowlings providing complete accessibility to the controls and drive components
    • Swivelling front wheel provided with tow bar attachment
    • Quick opening hinged inspection doors to allow visual check of engine oil levels and maintenance inspection points
    • Grounding points
    INTERIOR 2
    • Air conditioning Garret ECU
    • Primer finished cabin walls
    • Vibration dampers installation
    MISCELLANEOUS
    • Air intake/exhaust covers
    • Pitot tubes covers
    • Tie-down fittings provisions
    • Flight manual and technical publications
    • Ground tools Kit, including:
    • Tow bar
    • Lifting tool
      Wheel chocks
      2 The standard configuration does not include interior completion/mission equipment.
      Refer to para 2 for these additional equipments.
    EXTERIOR FINISHING
    • Finishing in accordance with manufacturer specification NTA 893 A
    • Primer exterior painting
    TRANSMISSION DRIVE SYSTEM
    • 900 SHP for take off and continuous operation main transmission
    • Two stage transmission
    • Two free wheeling units
    • Two transmission mounted hydraulic pumps with separate reservoir
    • Internal dry sump transmission lubrication with pressure and scavenge pump, and oil filter
    • Transmission oil chip detectors (2)
    • Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detector
    • Transmission cooling and lubrication system
    • Transmission shafts (engines to transmission, transmission to tail rotor, engines to blowers)
    INTERIOR ARRANGEMENT
    • Reclined rear cabin bulkhead
    • Two individual pilot seats, fore and aft adjustable, with lap belts
    • Aluminium alloy honeycomb reinforced floor with anti skid finish
    • Ventilation ram air inlets
    • Anti reflection instrument panel
    ELECTRICAL
    • 24 volt DC nickel cadmium battery with temperature probe
    • 160 Ampere self cooled starter generators (2)
    • Voltage regulators (2)
    • Battery relay
    • Interconnecting bus relay (2)
    • External power relay
    • Distribution buses (1 battery, 2 essential, 2 main)
    • External power receptacle
    • Position lights
    • Anti collision lights (2)
    • Taxing lights (2) and landing lights (2) on landing gear sponsons
    • Utility cockpit lights (2)
    • Instrument lights with dimming switch
    • Radio master switch
      POWER PLANT AND FUEL SYSTEM
      • Pratt & Whitney PW206C engine (2) or Turbomeca Arrius 2K1 engine (2)
      • Engine mounted fuel pump and filter assembly
      • Engine mounted oil pump and filter assembly
      • Engine mounted fuel control and governor (FMU)
      • Full Authority Digital Electronic Control (FADEC)
      • Lubrication and cooling system
      • Engine oil chip detectors (2)
      • Engine control panel
      • Fuel system control panel
      • RH refuelling point
      • Airframe mounted easy access fuel filter
      • Three fuel cells (160 USG)
      • Submerged fuel boost pump (2)
      • Ground fuel drains
      CAUTION & WARNING ADVISORY
      • Master warning lights
      • Master caution lights
      • Warning, caution & advisory messages (on IDS displays)
      • Engine fire detection system
      • Aural Warning Generator system
        ROTORS AND CONTROLS
        • Titanium metal main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite blades, swept tips, and dampers.
        • Steel metal tail rotor hub, corrosion protected, delta hinged type, semi–rigid, with two composite blades – individually interchangeable
        • Cyclic and collective controls powered by two hydraulic systems
        • Hydraulically powered anti torque system
        • Adjustable friction devices on cyclic and collective system
        • Force trim and artificial feel system
        • Adjustable directional control pedals
        • Dynamic flapping stop mechanism
          NAVIGATION INSTRUMENT – PILOT
          • Magnetic compass indicator
          INDICATIONS (ON IDS DISPLAY)
          • Dual gas generator speed (N1%)
          • Dual turbine outlet temperature (TOT °C)
          • Dual torque meter (TRQ%)
          • Dual power turbine speed (N2%)
          • Rotor speed (NR%)
          • Transmission oil temperature (°C) and pressure (PSI)
          • Two engine oil temperature (°C) and pressure (PSI)
          • Two fuel pressure (PSI)
          • Two fuel quantity (kg)
          • Two flight controls hydraulic system pressure (PSI)
          • Two utility hydraulic system pressure (PSI)
          • Outside air temperature (°C)
          • Two engine fuel flow (kg/hr)
          • Dual DC ammeter
          • Dual DC voltmeter
          • Dual AC voltmeter
          ADDITIONAL EQUIPMENT LIST
          • 8 Bose series X headsets
          • Baggage Comp. Extension (2.3m)
          • WX Radar RD 2000
          • TAS SKY 497 BF Goodrich
          • 221 gal. aux. fuel tank
          • Pulsed chip detector
          • Reinforced windshield
          • Metallic Color Series 500 (in lieu solid colours)
          • Customised Paint Scheme 2-3 colours
          • Super Silent Sound Proofing (old Paulstra Sound Proofing)
          • RH Electrically Operated Passenger Step
          FLIGHT INSTRUMENTS – PILOT
          • Barometric encoding altimeter
          • Air speed indicator
          • Instantaneous vertical speed indicator
          GENERAL INSTRUMENTS
          • Clock, 8 days and elapsed time