Leonardo AW169

Navigation

• Three Rockwell Collins Display Units 10” X 8” color AMLCD with LED backlight and NVIS compatibility:
• 2 Primary Flight Displays and 1 Multi-Function Display
• Integrated Standby Instrument System (ISIS)
• Two Display / cursor Control Panels/Devices (DCP/CCD)
• Reversionary Control Panel(RCP)
• Two Master Caution / Warning Lights (MCL/MWL)
• Two Avionics Full Duplex Ethernet (AFDX) switches
• Two Aircraft Monitoring & Management Computers (AMMC)
• Data TransferDevice(DTD)
• Two touch screen control panels
• Four Axis Automatic Flight Control System (AFCS)
• Two Flight Control Computer (FCC)
• Flight Control System (FCS) Control Panel
• TwoVHF-AM radios
• Two NAV (VOR/ILS/MB) receivers
• OneADF / DME
• Transponder with Enhanced Surveillance Mode (Mode S)
• First SBAS GNSS (GPS)
• Second SBAS GNSS (GPS)
• Two Audio Control Panels (Pilot and Co-pilot stations)
• Audio Management Unit interfacing external transceivers
• Passenger Intercom Amplifier
• Two flux valves
• Two Air Data and Altitude Heading Reference Systems (ADAHRS)
• Dual Radar Altimeter
• Pilot Clock/Co-Pilot Clock
• Moving map
• Health and Usage Monitoring System (HUMS)
• Flight Data Monitoring system (FDM)
• Helicopter Terrain Avoidance and Warning System (HTAWS)
• Synthetic Vision System (SVS)
• Enhanced Vision System –MaxVizEVS-1500
• TCAS III
• ADS-B Out
• Rotor brake system
• One solid state Cockpit and Voice Flight Data Recorder with ULB
• One Emergency Locator Transmitter (ELT –3 frequencies) (fixed)
• Approach plates chart holders with lights for pilot and co-pilot
• Co-pilot hinged window (storm window)

Communications