2016 Agustawestland Philadelphia Agusta Aw119MkII KX Turbine Helicopter

Description

• AW119Kx CONFIGURATION
• 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), 10 m opening, with jettisonable windows
• Passenger short foot step (LH & RH)
• Acrylic windshield and side windows
• Overhead cockpit transparent windows
• Lower cockpit transparent 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
• 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
• Power Plant and Fuel System
• Pratt & Whitney Canada PT6B-37A turbo-shaft 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 US gal)
• Submerged fuel pumps (2 boost and 1 transfer pump)
• RH refuelling point
• 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
• 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 (NVG compatible)
• 250 W landing lights (2)
• Anti-collision lights (2) (NVG compatible)
• Cockpit utility lights (2) (NVG compatible)
• Instrument lights
• Radio master switch
• Avionic Package
• Depending on both contractual delivery date and Country of destination, the AW119Kx helicopter could be delivered with EASA/FAA Type Certification or could be equipped with Garmin G1000HTM approved as FAA STC.
• The latter does not include the magnetic compass indicator.
• Garmin G1000HTM Integrated Flight Deck system comprising:
• Two GDU-1040 4” display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating:
• Radio tuning controls
• Flight Management System (FMS)
• Synthetic Vision System
• Helicopter Terrain Awareness and Warning System (HTAWS)
• Two GEA-71H Aircraft Interface Unit
• Two GSC-46 Signal Conditioners
• GRS-77H AHRS
• GDC-74H Air Data Computer (ADC)
• NAV 1&2
• GPS 1&2
• Aural Alert Generator
• ADF interface
• DME tuning interface
• GTX-33H Mode-S Transponder with Extended Squitter (ES) capability
• Radar Altimeter RA-4500 FreeFlight Systems
• Digital Audio Control System (DACS) COBHAM with two cockpit panels
• Magnetic Compass indicator
• L3 Avionics System ESI-2000 Electronic Standby Indicator
• Engine Hour meter
• Systems Data (on PFD/MFD)
• 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 (on MFD)
• Engine oil pressure (PSI) and temperature (°C) indicator (on MFD)
• Fuel pressure (PSI) (on MFD) and fuel quantity (kg) indicator (on PFD/MFD)
• Two hydraulic pressure system indicators (PSI) (on MFD)
• Outside air temperature indicator (°C) (on PFD)
• DC voltmeter (VDC) (on MFD)
• DC ammeter (Amp) (on MFD)
• Central Warning System (CWS)
• Master warning lights
• Master caution lights
• Warning, caution and advisory messages on PFD display
• Aural alerts from IAU 1 & 2
• Interior Arrangement
• Pilot and co-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
• Exterior Finishing
• Finishing in accordance with manufacturer specification
• Miscellaneous / Ground 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 (main rotor retention straps)
• Standard Equipment
• 28 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
• Additional Avionic Equipment
• AC power supply system (2 inverters)
• AFCS 3-axis duplex SP-711 Honeywell
• Additional Equipment
• Baggage compartment extension (1.9 m)
• (*) It may be affected by avionic customization
• Dual controls
• Fuel cap with key-lock
• Reinforced windshields (pilot and co-pilot)
• Rotor brake
• Sliding windows on cockpit doors
• Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
• Interior Trim
• Bleed air heater
• Primer finished cabin walls
• Interior Equipment –