Pilatus PC-24

Pilatus Advanced Cockpit Environment (ACE™): Two (2) Primary Flight Displays (PFD), Flat Panel Display Unit, 12” diagonal SmartView™ Synthetic Vision System on PFD Two (2) PFD Controllers Two (2) Integrated GNSSU SBAS Receivers 2 Audio/Marker Panels Dual Channel Auto-Pilot with Dual Yaw Damper Flight Guidance Panel Two (2) Multifunction Displays (MFD), Flat Panel Display Unit, 12” Diagonal Multifunction Controller (MFC) including Alphanumeric Keyboard and Joystick Cursor Control Device (CCD) Switch Panels Two (2) Mode S Diversity Transponders with ADS-B Out Two (2) Multi-Mode Digital Radios (MMDR) Attitude Reference Systems comprising of One (1) IRS and One (1) AHRS lDME Radar Altimeter CPDLC Capability Integrated Enhanced Ground Proximity Warning System (EGPWS) Class A Traffic Alert Integrated Traffic Collision Avoidance System (TCAS II) Auto-Throttle System Utilities Management System Two (2) Pitot-Static Systems Two (2) Angle-of-Attack (AOA) Sensors RDR 2100 Weather Radar Electronic Standby Instrument System (ESIS) ELT 406 MHz w/ Remote Switch, GPS & NAV Interface Flight Time Recorder (“Hobbs Meter”)

Interior
Configuration: Eight (8) Passengers Galley Location: Forward Lavatory Location: Forward Cabin: Six (6) Single Deluxe Seats, Followed by Two (2) Commuter Seats Connectivity: AEROWAVE 100 Inflight-Internet Entertainment: USB Outlets, Int. Cabin Management System including IFE