2018 LEONARDO AW119MKII

2018 Leonardo AW119MKII Helicopter

Standard Equipment
– 28-volt battery
– 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 Equipment
– Baggage compartment extension (1.9 m)
– 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

Additional Avionic Equipment
– AC power supply system (2 inverters)
– Stability Augmentation System  

Engine & Mods

Power plant & 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
– 4-cell fuel system (711 l – 188 USgal)
– Submerged fuel pumps (2 boost and 1 transfer pump)
– RH refueling point  

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
– Passenger short footstep (LH & RH)
– Acrylic windshield and side windows
– Overhead cockpit transparent windows

– Lower cockpit transparent windows
– Removable fiberglass 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 point 

Avionics & Equipment

Avionic package:
– Garmin G1000H Integrated Flight Deck system comprising:
• Two GDU-1040 10.4” 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 with integral Central Maintenance Computer
(CMC) GEA-71H
•Two GSC-46 Signal Conditioners
•GRS-77H AHRS
•GDC-74H Air Data Computer (ADC)
•Two GIA-63H Integrated Avionics Units (IAU) comprising:
COM 1&2
NAV 1&2
GPS 1&2
Aural Alert Generator
DME tuning interface
•GTX-33H Mode-S Transponder with Extended Squitter (ES) capability
– Radar Altimeter RA-4500 FreeFlight Systems
– Digital Audio Control System (DACS) NAT with two cockpit panels
– Magnetic Compass indicator
– L3 Avionics System ESI-2000 Electronic Standby Indicator Airframe Hour meter
g. Systems data (on MFD/PFD) 

– 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 PDF display – Aural alerts from IAU
1 & 2

Interior

– Leatherette seats
– Soundproofing
– 3-point shoulder harness with inertial reels and safety belts for aft cabin seats
– Cargo net provisions

 Aft cabin sliding passenger doors RH & LH
– Cabin loudspeakers

Exterior

• Main rotor blades high visibility painting

Avionic package:
– Garmin G1000H Integrated Flight Deck system comprising:
• Two GDU-1040 10.4” 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 with integral Central Maintenance Computer
(CMC) GEA-71H
•Two GSC-46 Signal Conditioners
•GRS-77H AHRS
•GDC-74H Air Data Computer (ADC)
•Two GIA-63H Integrated Avionics Units (IAU) comprising:
COM 1&2
NAV 1&2
GPS 1&2
Aural Alert Generator
DME tuning interface
•GTX-33H Mode-S Transponder with Extended Squitter (ES) capability
– Radar Altimeter RA-4500 FreeFlight Systems
– Digital Audio Control System (DACS) NAT with two cockpit panels
– Magnetic Compass indicator
– L3 Avionics System ESI-2000 Electronic Standby Indicator Airframe Hour meter
g. Systems data (on MFD/PFD) 

– 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 PDF display – Aural alerts from IAU
1 & 2