Agusta A109E Power
260 horas totais | ano de 2009
Helicóptero bi-turbina de maior sucesso em sua categoria.
Autonomia: 948 km
Velocidade máxima de cruzeiro: 287 km / h
Assentos: 1 piloto + 7 passageiros
Características
Destaques
- Internado temporariamente com impostos recolhidos até 2014 Arrendamento Operacional
- Horas totais de Célula: 260
- 657 Landings
- Engines:
- Engine # 1: Total Time: 260 hs – Cycles: 548
- Engine # 2: Total Time: 260 hs – Cycles: 546
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
EQUIPAMENTOS OPCIONAIS INSTALADOS
- 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