When the Falcon 7X overhead panel experiences a short circuit on a protected function output, what action is taken by the overhead panel monitoring logic?, The affected channel is electrically isolated and all commands associated with that channel remain inhibited until aircraft power is cycled., The fault is transmitted over the Aeronautical Radio, Incorporated (ARINC) 429 maintenance line and the suspected output is opened; the associated function must then be completely cycled to restore the output once the short circuit has cleared., The applicable power supply module is disconnected and the remaining two power supplies automatically assume control of both overhead-panel channels., Within a Modular Avionics Unit (MAU), what is the primary architectural purpose of the dual-channel Generic Input/Output (I/O) modules?, Each channel independently performs the complete avionics application processing and votes with the Network Interface Controller/Processor modules before transmitting data., Both channels are connected to the same Virtual Backplane Peripheral Component Interconnect (VbPCI) channel so that either channel can provide duplicated processor outputs., One channel connects to VbPCI channel A and the other to channel B, with input information received by one channel automatically transmitted to the second channel, allowing data availability to be maintained if power to one channel is lost., What is the primary function of the Network Interface Controller/Processor modules within the Falcon 7X Enhanced Avionics System (EASy)?, They provide the gateway between the Virtual Backplane Peripheral Component Interconnect (VbPCI) bus inside each Modular Avionics Unit and the Avionics Standard Communication Bus, Version D (ASCB-D), while also providing network synchronization and monitoring functions., They generate all display symbology and directly drive the Primary Display Units and Multifunction Display Units through the Fibre Channel Bus., They convert all analog and discrete aircraft inputs directly into Aeronautical Radio, Incorporated (ARINC) 429 format before transmission to the processor modules., During operation of the Synthetic Vision System (SVS), what occurs if the three-dimensional aircraft position becomes invalid?, The Synthetic Vision background remains displayed but all runway and obstacle data are removed while the attitude background remains unchanged., The Synthetic Vision layer progressively fades out over approximately two seconds, is replaced by the normal blue/brown background, and an amber reverse-video “SV POS” annunciation is displayed., The Synthetic Vision System freezes the last valid terrain image until valid Flight Management System position information becomes available again., What is the function of the Data Acquisition System within the Falcon 7X Enhanced Avionics System?, It provides only the physical interface between the flight-data recorders and the Modular Avionics Units., It performs all display generation functions and controls the Fibre Channel Bus between the Advanced Graphics Modules and cockpit displays., It acquires data from other avionics systems, manages the Avionics Standard Communication Bus, Version D (ASCB-D), maintains aircraft configuration and system time/date, provides bus isolation and coupling, and supports software and database loading., Within each Modular Radio Cabinet, what is the principal function of the Network Interface Module (NIM)?, It converts and transfers control and status information between the Avionics Standard Communication Bus, Version D (ASCB-D) and the internal Radio Control Bus, and also performs analog-to-digital conversion between analog radio audio inputs and the digital audio bus., It directly generates radio-frequency transmission signals for the Very High Frequency, Automatic Direction Finder and Distance Measuring Equipment systems., It supplies only aircraft configuration information to the radio modules through its Aircraft Personality Module and has no active data-conversion function., How is a radio tuning command entered through the Primary Display Unit normally transferred to the applicable radio module in the Modular Radio Cabinet?, The tuning command is sent directly from the Primary Display Unit to the radio module through an Aeronautical Radio, Incorporated (ARINC) 429 connection., The tuning command is converted by the Advanced Graphics Module into a discrete electrical command and sent directly to the applicable Line Replaceable Module., The tuning information is transmitted over the Avionics Standard Communication Bus, Version D to the Network Interface Module, processed by its radio processor, and then sent to the applicable radio module through the Radio Control Bus., At aircraft power-up, how is the master Monitor Warning function selected from the three operating Monitor Warning instances?, Monitor Warning 3 becomes master first after approximately 500 milliseconds, followed by Monitor Warning 2 and then Monitor Warning 1 if the previous instance fails., Monitor Warning 1 becomes master after approximately 500 milliseconds if no other master exists; Monitor Warning 2 attempts at approximately 700 milliseconds and Monitor Warning 3 at approximately 900 milliseconds., All three Monitor Warning instances remain equal masters and each independently commands one display unit., What occurs when the Flight Data Recorder/Cockpit Voice Recorder acceleration contact senses an acceleration greater than approximately 3 g?, The acceleration contact closes its circuits and energizes the recorder acceleration relay, removing power from the Flight Data Recorder/Cockpit Voice Recorder unit so that audio recording is stopped., The recorder automatically switches from normal recording to a protected high-speed recording mode and doubles the flight-data sampling rate., Only the Cockpit Voice Recorder microphone inputs are isolated while the Flight Data Recorder continues operating from an internal battery., On a Falcon 8X compared with the earlier Falcon 7X Enhanced Avionics System architecture, which statement correctly describes one of the significant Enhanced Avionics System III changes?, The Falcon 8X eliminates the Modular Avionics Units and replaces them with independent federated avionics computers connected only by Aeronautical Radio, Incorporated 429 buses., The Falcon 8X retains the original Network Interface Cards and Avionics Standard Communication Bus, Version D architecture but removes Synthetic Vision System capability., The Falcon 8X Enhanced Avionics System III incorporates modified Modular Avionics Units, upgraded Network Interface Controllers, an enhanced Avionics Standard Communication Bus, software and database changes, and uses Synthetic Vision System together with Enhanced Flight Vision System as the Combined Vision System.

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