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Questions and Answers
What information does the LEVER ON provide to the RA?
What information does the LEVER ON provide to the RA?
- Engine thrust levels
- Fuel consumption rates
- Engine power ON/OFF status (correct)
- Flight altitude adjustments
What does DME provide when connected to both selected ground stations?
What does DME provide when connected to both selected ground stations?
- Navaid location coordinates
- Navigation waypoint data
- Morse audio identification (correct)
- Flight path visualization
Where is VOR and Marker information displayed?
Where is VOR and Marker information displayed?
- Autopilot control panel
- Engine Indication and Crew Alerting System (EICAS)
- Central Maintenance Computer (CMC)
- Primary Flight Display (PFD) and Navigation Display (ND) (correct)
What indication represents Auto Tune mode in Radio Navigation tuning?
What indication represents Auto Tune mode in Radio Navigation tuning?
What does Manual Tune mode indicate in Radio Navigation tuning?
What does Manual Tune mode indicate in Radio Navigation tuning?
What indication represents Backup Tuning mode in Radio Navigation tuning?
What indication represents Backup Tuning mode in Radio Navigation tuning?
What are the interfaces for the AESS responsible for?
What are the interfaces for the AESS responsible for?
Which element provides the crew with critical navigational information?
Which element provides the crew with critical navigational information?
What happens when the INT/RAD switch is in the INT position?
What happens when the INT/RAD switch is in the INT position?
How can one activate the transmission mode for the selected radio set using the INT/RAD switch?
How can one activate the transmission mode for the selected radio set using the INT/RAD switch?
What indicates that logon is confirmed in SATCOM?
What indicates that logon is confirmed in SATCOM?
What occurs when there is a failure indication of RMP?
What occurs when there is a failure indication of RMP?
What does the red light on the RMP signify during a failure?
What does the red light on the RMP signify during a failure?
What is the purpose of the dialog bus in RMP operations?
What is the purpose of the dialog bus in RMP operations?
How does the INT/RAD switch function when it is in the RAD position?
How does the INT/RAD switch function when it is in the RAD position?
What is the consequence of operating RMPs in degraded mode?
What is the consequence of operating RMPs in degraded mode?
Which unit receives discrete signals from the dimming unit?
Which unit receives discrete signals from the dimming unit?
What is the role of DEU B in the cockpit?
What is the role of DEU B in the cockpit?
How many IBUs can DEU A transmit lighting requests to at maximum?
How many IBUs can DEU A transmit lighting requests to at maximum?
How are cabin lighting scenarios loaded?
How are cabin lighting scenarios loaded?
Which interface is used by DEU A to transmit lighting requests?
Which interface is used by DEU A to transmit lighting requests?
What is one function of the lighting control system in aircraft?
What is one function of the lighting control system in aircraft?
Where can users display the ACR status and initialization parameters?
Where can users display the ACR status and initialization parameters?
What triggers the wireless airport communication system to turn on?
What triggers the wireless airport communication system to turn on?
What does the WLM check before triggering the 'power ON/OFF' signal?
What does the WLM check before triggering the 'power ON/OFF' signal?
How can the operational status of the CVR be confirmed?
How can the operational status of the CVR be confirmed?
What preliminary condition must the WLM verify for wireless communication to operate?
What preliminary condition must the WLM verify for wireless communication to operate?
What is indicated by the 600 Hz tone during the CVR system test?
What is indicated by the 600 Hz tone during the CVR system test?
What can the GATELINK P/BSW do regarding the WACS?
What can the GATELINK P/BSW do regarding the WACS?
What action must be taken to initiate the CVR system test?
What action must be taken to initiate the CVR system test?
What is the effect on cabin general lighting during a total loss of the serial data bus system?
What is the effect on cabin general lighting during a total loss of the serial data bus system?
What action causes lavatory lightings to switch to 100% brightness?
What action causes lavatory lightings to switch to 100% brightness?
What happens to cabin general lighting in the event of cabin decompression?
What happens to cabin general lighting in the event of cabin decompression?
What occurs independently of any light settings during CIDS loss?
What occurs independently of any light settings during CIDS loss?
Which of the following scenarios will NOT result in the lighting dimming to 50%?
Which of the following scenarios will NOT result in the lighting dimming to 50%?
Which system failure is related to the dimming of cabin general lighting?
Which system failure is related to the dimming of cabin general lighting?
What does 'FAP' stand for in the context of the document?
What does 'FAP' stand for in the context of the document?
What is the primary purpose of switching lavatory lightings to 100% brightness?
What is the primary purpose of switching lavatory lightings to 100% brightness?
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Study Notes
Airbus A380 (EA GP7200 & RR RB211 Trent 900) B1/B2 Engineering Training Study Guide
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LEVER ON Functionality: Provides engine power ON/OFF information to the RA, inhibiting interactive mode during flight.
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DME Connection: Linked to AMUs for morse audio identification from selected ground stations, aiding crew navigation.
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VOR and Marker Display: Information shown on Primary Flight Display (PFD) and Navigation Display (ND).
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Radio Navigation Auto Tune Indication: None displayed when in Auto Tune mode.
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Radio Navigation Manual Tune Indication: "M" underlined and dimmed appears near the navaid on NDs during Manual Tune mode.
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Radio Navigation Backup Tune Indication: "R" underlined and dimmed displayed for Backup Tuning.
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AESS Interfaces: EFIS control panels manage different viewing modes on Navigation Displays (NDs).
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INT/RAD Switch Functionality:
- In INT position, enables stable flight interphone transmission.
- In RAD position or when using PUSH TO TALK, activates radio set transmission mode.
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SATCOM Logon Confirmation: Indicated by a green LOGGED ON AUTO or LOGGED ON MANUAL on the SATCOM CONFIG page.
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RMP Failure Indications: Degraded mode operational if system defects occur; warnings displayed on EWD, with a red light indicating crew action is required.
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ACR Status Display: Users can view ACR status, initialization parameters, communication means, and ACARS network status through RMPs.
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Wireless Airport Communication System: On "radio power enable", WLM checks aircraft ground status and triggers "power ON/OFF" if capable, with GATELINK P/BSW able to deactivate WACS.
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CVR Test and Erase Function: Ground test initiated by pressing TEST pushbutton, with audible tone confirming operational status (600 Hz through boomset).
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Dimming Unit Signals: Discrete signals received by ECAM CONTROL panel for lighting adjustments.
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DEU B Connections: Manages cockpit indicators and stand-alone signs for lavatories located at door M1L.
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Cabin Lighting Scenarios: Loaded in CAM as per airline specifications for tailored lighting experiences.
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DEU A Capability: Each DEU A transmits lighting requests to a maximum of 8 IBUs using a modified RS485 interface.
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Loss of CIDS Responses: In case of failure, cabin general lighting automatically dims to 50%, triggered by loss of data bus, FAP malfunction, or CIDS issues.
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Cabin Decompression Response: General cabin lighting brightens to 100% upon cabin decompression for safety.
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Lav Lightings for Maintenance: Activated to 100% brightness from the "LAV MAINT" push button on the FAP hard key panel for cleaning and maintenance.
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