HELICÓPTERO 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

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 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

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