2013 G650 AVIONICS AND EQUIPMENT Integrated Digital Avionics System, including: four (4) flat-panel LCD Electronic Display Units triple Modular Avionics Units (MAUs) a Guidance Panel dual Standby Multifunction Controllers (SMC) three (3) Multi-Function Control Display Units (MCDUs) dual Cursor Control Devices (CCDs) Primary sensors consisting of: four (4) Multifunction Air Data Probes (MFPs) triple Inertial Reference Systems (IRS) dual Global positioning Systems (GPS) Head Up Display Enhanced Vision System Dual Loading LAN Management Unit Cockpit Printer Communications and Navigation Systems, including: Minimum Navigation Performance (MNP) Reduced Vertical Separation Minimums (RVSM) FANS I/A oceanic position reporting and communication three (3) Multi- Function Control Display Units (MCDUs) Dual HF Transceivers Triple VHF through two (2) VHF transceivers and one (1) NAVCOM unit VHF Navigation, Instrument Landing System (ILS), and Marker Beacon Automated Direction Finder (ADF) Dual (MODE S) ATC transponders Traffic Collision Avoidance System (TCAS) Dual Distance Measuring Equipment (DME) Transceivers Three-dimensional (3D) color weather radar system Dual digital radio altimeters Satellite Communications System (SATCOM) ASC003 SATCOM Direct Datalink Service Provider Enhanced Ground Proximity Warning System (EGPWS) Emergency Locator Transmitter (ELT) ASC007 Weather Radar with Predictive Wind Shear Next Generation Radar (NEXRAD) Flight Data Recorder System (FDR) Cockpit Voice Recorder (CVR) Central Maintenance Computer (CMC) FAR Part 135 compliant CABIN/INTERIOR Forward Left-Hand Cabinet Forward Right-Hand Closet/Storage Cabinet Crew Rest Compartment (Forward RH), induding One (1) RCO Engineering Inc. manually operated single seat Forward Lavatory Forward Cabin Bulkheads with Pocket Door Mid Cabin Bulkheads with Pocket Door Aft Cabin Bulkheads and Door Forward Galley/Galley Annex, including: Crystal storage in lighted c