2016 Agusta AW169

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 Transfer Device (DTD) • Two touch screen control panels • Four Axis Automatic Flight Control System (AFCS) • Two Flight Control Computer (FCC) • Flight Control System (FCS) Control Panel • Two VHF-AM radios • Two NAV (VOR/ILS/MB) receivers • One ADF / 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 – MaxViz EVS-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