AW109 TREKKER 2019












R$ sob consulta
GP3254
Faixa de preço: R$3,5 milhões a R$10 milhões (US$700k to US$2mi)
- Categoria: HELI BITURBINA
- Fabricante: AGUSTA WESTLAND
- Ano de fabricação: 2019
- Assentos: 08
- Horas totais de célula: 80
- Aceita permuta: Não
- Aeronave: Disponível
- AR CONDICIONADO
Descrição da aeronave
Helicóptero AW109 Trekker 2019 à venda
Airframe
Aluminium alloy and bonded panel fuselage Semi-monocoque aluminium alloy tail boom
New reinforced skid type landing gear
Two hinged jettisonable crew doors (LH and RH)
Two 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 acessibility to the controls and drive components
Quick opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points
Grouding points
Jacking and hoisting points
Rotors and Controls
Titanium main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite material blades, swept tips, and dampers
Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite material 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
Flapping and droop restraint mechanism
Power Plant and Fuel System
Two Pratt & Whitney Canada PW207C turbo-shaft engines
Two independent electronic control systems (FADEC) with normal emergency and training operation modes and auto-start
Engine mounted fuel pump and filter assembly (2)
Engine mounted oil pump and filter assembly (2)
Engine mounted fuel control and governor (2)
Lubrification and cooling system
Engine oil chip detectors (2)
Engine control panel
Two independent fuel systems with cross-feeding valve and control panel
3 cell crash-resistant fuel system (575 l – 152 USgal)
Submerged fuel boost pumps (2)
Airframe mounted easy access fuel filter
RH refuelling point
Ground fuel drains
Transmission Drive System and Hydraulic System
960 shp for takeoff and 900 shp continuous operation mains transmission
Three-stage transmission
Free wheeling units (2)
Dual independent, redundant hydraulic systems
Transmission mounted hydraulic pumps (2) 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 90º gear box including oil level sight glass and chip detector
Transmission cooling and lubrication system
Transmission shafts
Electrical System
24 V DC Ah nickel-cadmium battery with temperature probe
200 A self-cooled starter generators (2)
Voltage regulators (2)
Battery relay
Interconnecting bus relays (2)
External power relay
Distribution buses (1 battery, 2 essential, 2 emergency, 2 main, 2 auxiliary)
External power receptacle
Position lights (NVG friendly – green, red, white)
Taxing lights (1RH) and landing lights (1 LH)
Anti collision lights (2) (NVG friendly)
Cocpit utility lights (2)
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)
Painting
Standard colour scheme from Company paint selection, solid colour
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 supply system (2 inverters)
AFCS 3-axis duplex SP-711 Honeywell
Radar altimeter
Doors key lock
Airframe hourmeter
Baggage compartment lights
Crew open door actuators
Engine compartment fire extinguishers (Qty 2)
Fuel cap whith key-lock
Pulsed chip detectors (in lieu of quick disconnecting chip detectors)
450 W Retractable/ rotating landing light (nose mounted)
Miscellaneous/ Ground Equipment
Air intake/ exhaust covers
Ground tools kit (including tow bar, ground wheels, lifting tool)
Pilot tubes covers
Rotorcraft Flight Manual (RFM) and technical publications
Tie-down fittings (main rotor retention straps)
Customer Required Configuration
Interior Equipment – Cabin
- Utility Interior (Rigid liners)
- Passenger cabin
- All seats crash – resistant covered with leatherette
- 3 fwd facing seats (aft bench) with seating modules individually removable
- 3 aft facing seats (central bench) with seating modules individually removable
- 4-point shoulder harness with inertial reels and safety belts for all seats
- Liners
- Intercommunication system for passengers
- Cabin loudspeakers (Qty 2)
- Reading lights, emergency lights
- Upper and lower air vents
- Headset H10-13H David Clark (Qty 6)
- Cockpit equipment
- Standard cockpit interior
- Soundproofing
Avionics Equipment
Dual Pilot IFR package (in addition to Single Pilot VFR STD configuration)
Dual Controls
Co-Pilot large colour Primary Flight Display (PFD) – Genesys, embeldding:
- Synthetic Vision System (SVS)
- Highway In The Sky (HITS)
- Helicopter Terrain Awareness and Warning System (HTAWS)
- Flight Management System (FMS)
- Rdio tuning controls
2 nd VHF/AM
2 nd VOR/ILS
2 nd GPS
DME
Marker beacon
Electronic Standby Indicator
Co-Pilot Intercommunication System (ICS)
Dual Master warning lights
Dual Master caution lights
2 nd Magnetic Compass indicator
Digital clock
Flight Director
Utility Equipment
Air conditioning
213 USgal crash-resistant fuel system (in lieu of 152 USgal)
Baggage compartment extension (2.3m)
Rotor brake
Utility power socket 12 VDC up to 8 Ah
Utility pocket behind pilot and co-pilot seats
(*) Not compatible with Pilot and co-pilot multipurpose holder
Cargo hook (1400 Kg) – provision
(*) Requires either the rear view mirror or the cargo hook camera
Removable Equipment
Set of six VIP pax seat cushions
The above aircraft is third party and as such subject to prior sale and / or price change. Data provided by owner, subject to verification.
A aeronave acima é de terceiro e como tal sujeita à venda prévia e/ ou alteração de preço. Dados fornecidos pelo proprietário, sujeitos à verificação.
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