Agusta AW119Ke Koala

423 horas totais | ano 2011

Vendido

Capaz de decolar com o tanque cheio e com todos os assentos ocupados.

Autonomia: 935 km

Velocidade máxima: 258 km/h

Assentos: 1 piloto + 7 passageiros

Características

Destaques

Aeronave 100% internada com todos os impostos de importação pagos.
Sem histórico de acidentes.
Único dono.
Horas Totais:
Célula: 423 hrs
Motores: 423 hrs

Hélicóptero Agusta AW119 KE Koala(FAA/EASA) VFR Standard Configuration

1. BASIC AIRCRAFT
a. 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 & RH)
Two sliding passenger doors (LH and RH), 1.10 m opening, with jettisonable windows
Acrylic windshield and side windows
Acrylic overhead windows
Removable fibreglass tail rotor gearbox fairing
Quick removable tail rotor drive shaft cover
Separate baggage compartment with hinged door
Three jacking points
Removable fairing and cowlings, for complete accessibility to the controls and drive components
Quick opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points
Grounding points
b. 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 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
c. Power plant and fuel system:
Pratt & Whitney Canada PT6B-37A turboshaft engine
Engine mounted fuel pump and filter assembly
Engine mounted oil pump and filter assembly
Engine mounted fuel control and governor
Electronic Engine Control (EEC)
Lubrication and cooling system
Engine oil chip detector (1)
Engine mounted fuel heater
Fuel system control panel
3-cell fuel system (605 l – 160 USG)
Submerged fuel pumps (2 boost and 1 transfer pump)
RH refuelling point
d.Transmission drive system and hydraulic system:
917 shp for take off and 900 shp continuous operation main transmission
Two-stage transmission
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 90° gear box including oil level sight glass and chip detector
Transmission cooling and lubrication system
Transmission shafts
e. Electrical system:
28 V DC 22 Ah nickel-cadmium battery with temperature probe
200 A self-cooled starter generator
Voltage regulator
Battery relay
Interconnecting bus relay
External power relay
Distribution buses (2)
External power receptacle
Position lights
250 W landing lights (2)
Anti collision lights (2)
Cockpit utility lights (2)
Instrument lights with dimming switch
Radio master switch
f. Flight instruments – pilot:
Airspeed indicator
Barometric encoding altimeter
Vertical speed indicator
Magnetic compass indicator
Clock, 8 days and elapsed time
Dual tachometer backup instrument
g. Instrumentation (on IDS display):
Inter turbine gas temperature indicator (ITT°C)
Engine torque indicator (TQ%)
Compressor speed indicator (N1%)
Turbine speed indicator (N2%)
Rotor speed indicator (NR%)
Transmission oil pressure (PSI) and temperature (°C) indicator
Engine oil pressure (PSI) and temperature (°C) indicator
Fuel pressure (PSI) and fuel quantity (kg) indicator
Two hydraulic pressure system indicators (PSI)
Outside air temperature indicator (°C)
Two AC voltmeters (VAC)
DC voltmeter (VDC)
DC ammeter (Amp)
h.Central warning system:
Master warning lights
Master caution lights
Warning, caution and advisory messages (on IDS displays)
Aural warning generator system
i. Interior arrangement:
Two individual pilot seats, fore and aft adjustable, with lap belts and headrests
Aluminium alloy honeycomb reinforced floor with anti-skid finishing
Ventilation ram air inlets
Anti reflection instrument panel
j. Exterior finishing:
Finishing in accordance with manufacturer specification (NTA 893 A)
Primer exterior painting

Standard Equipment

27 Ah battery (in lieu of 22 Ah battery)
Active Noise Reduction (ANR) headsets (pilot and co-pilot)
Baggage compartment lights
Crew open door actuators
First aid kit
Fuel drain electrical valves
Portable fire extinguisher
Quick disconnecting chip detectors
Shoulder harness with inertial reels (pilot and co-pilot)
Tail boom strake

VFR Avionic Package

ADF KR-87 Bendix/King
Gyrocompass C14A Honeywell
ICS pilot AG-06-1U Agusta/Gemelli
Pilot navigation instruments (including ADI & HSI)
Transponder (mode S) KT-70 Bendix/King
VHF-COM/GPS 250XL Garmin

Additional Avionic Equipment

AC power supply system (2 inverters)
AFCS 3-axis duplex SP-711 Honeywell

Additional Equipment

Baggage compartment extension (1.9 m)
Dual controls
Reinforced windshield (pilot and co-pilot)
Rotor brake
Sliders on cockpit doors windows
Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips

Interior

Bleed air heater
Primer finished cabin walls

Miscellaneous/Ground e Equipment

Air intake/exhaust covers
Ground tools kit (including tow bar, ground wheels, lifting tool)
Pitot tubes covers
Rotorcraft Flight Manual (RFM) and technical publications
Tie-down fitting provisions

Painting

Standard colour scheme from Company paint selection, solid colour

Optionals

EFDH-1000: Aspen
GNS-530AW – Garmin
Pulse Light P/S – Pulse Light
WX-500 Stormscope – L3
TRA-3500- Radar Altimeter – FreeFlight• PMA- 8000B Cx. Audio – PS Engineering
AA-82- Pax Audio Stereo – NAT
Display 7“ – Rosen
Airshow- Flight Display
Tel. s/ Fio – Aircell
GTX-327-ATC Digital – Garmin
TAS-605 – TCAS 13NM – Avidyne
Headphone A20 – Ipod – Bose
Headphone A20 – Ipod-Bluetooth – Bose
External Camera
DVD/CD/MP3 Player – Airshow
Interface Airshow/DVD/Cameras – AirshoW

AW119 MKII HELICOPTER BASIC CONFIGURATION DESCRIPTION INTERIOR COMPLETION/MISSION EQUIPMENT

1. Executive interior basic arrangement (including only soundproofing, seats benches, liners without painting, reading lights , advisory lights, cabin loudspeakers)
2. Air Conditioning
3. High visibility blades
4. Auxiliary fuel tank (5 cells 230 USGAL)
5. Sliding Windows in cabin
6. Baggage compartment extension 2.3m
7. Steps Long Boarding LH & RH
8. Inlet Barrier Filter
9. Cargo hook primary (1400 kg / 3086 lb) provision
10. Hour meter
11. Strobe lights on horizontal stabilizer
12. All weather covers (ground equipment)
13. ELT C406-2HM
14. Headset Pilot and Co-pilot Bose Serie 20 (in lieu of std David Clark)
15. Credit for Primer painting only