Indicating & Recording Flashcards
Q1 | RECORDER PANEL
When does the Digital Flight Data Recorder (DFDR) operate?
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- On the ground, for 5 minutes after electrical power is supplied to the aircraft
- When at least 1 engine is operating
- Continuously in flight, whether or not the engines are operating
- Stops 5 minutes after the last engine is shut down
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Q2 | RECORDER PANEL
What is the purpose of the DFDR EVENT pushbutton?
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Briefly pressing this button sets an event mark on the Flight Data Recorder
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Q3 | RECORDER PANEL
What would be indicated if the altitude window changed from yellow to amber?
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The aircraft has deviated from the FCU selected altitude or flight level by 250 feet
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Q4 | RECORDER PANEL
When is altitude alerting automatically inhibited in flight?
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- When slats are extended with the landing gear selected down
- On approach after glide slope capture
- When the landing gear is locked down
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Q5 | RECORDER PANEL
What does it mean when the altitude digits change from green to amber?
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The aircraft has descended below the MDA/DH entered into the FMGC
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Q6 | RECORDER PANEL
When is Radio Height displayed on the PFD?
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Below 2,500 feet AGL
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Q7 | RECORDER PANEL
What would a flashing amber ILS indicate on the bottom of the PFD?
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Flashes amber when APPR mode is armed and the LS display is not selected
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Q8 | RECORDER PANEL
Information from ILS receiver 1 is displayed where?
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- Captain’s PFD
- F/O’s ND
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Q9 | NAVIGATION DISPLAY
Top of Descent and Continue Descent arrows are displayed in blue or white. What is the difference?
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- Top of Descent – Always white (never armed)
- Continue Descent – Blue indicates armed, white indicates NOT armed
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Q10 | NAVIGATION DISPLAY
What color does each altitude constraint circle represent?
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- White – constraint is not taken into account
- Magenta – constraint is predicted to be satisfied
- Amber – constraint is predicted to be missed
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Q11 | NAVIGATION DISPLAY
If mode range data fails what should you expect to see on the ND?
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ROSE NAV mode at 80 nm range
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Q12 | ENGINE WARNING DISPLAY
What are the 3 levels of ECAM Failure Mode Notifications?
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Level 1 – ALERT:
- Associated with amber E/WD message, no aural signal, and requires crew monitoring
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Level 2 – CAUTION:
- Associated with the amber MASTER CAUT light, single chime, and require crew awareness
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Level 3 – WARNING:
- Associated with the red MASTER WARN light, CRC, and require immediate action
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Q13 | ENGINE WARNING DISPLAY
If simultaneous failures occur, how will they be presented to the crew?
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A level 3 Warning has priority over a level 2 Caution which has priority over a level 1 Alert
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Q14 | ENGINE WARNING DISPLAY
What types of failures are presented to the crew?
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IPS
- Independent – Failure affecting an isolated system/item without degrading other systems/items
- Primary – Failure of a system/item that affects the use of other systems/items
- Secondary – Loss of a system/item resulting from a primary failure
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Q15 | ENGINE WARNING DISPLAY
What indication does the E/WD provide for secondary failures?
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Secondary failures are displayed on the lower right portion of the E/WD and are preceded by an *
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Q16 | ENGINE WARNING DISPLAY
What does the appearance of a green arrow at the bottom of the E/WD screen indicate?
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Information has overflowed off the screen and the pilot must scroll down using the CLR pushbutton on the ECAM panel
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Q17 | ENGINE WARNING DISPLAY
What does the display of T.O. INHIBIT or LDG INHIBIT indicate?
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Most warnings and cautions are inhibited to avoid unnecessary distractions during critical phases of flight
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Q18 | ENGINE WARNING DISPLAY
When does the Takeoff Memo appear?
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- 2 minutes after the second engine is started or when the T.O. CONFIG TEST pushbutton is pressed with one engine running
- Takeoff Memo is removed when takeoff power is applied
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Q19 | ENGINE WARNING DISPLAY
When does the Landing Memo appear?
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- Below 2,000 feet RA
- Memo disappears after touchdown (80 knots)
- Displays at 800 feet if you never climbed above 2000 feet RA
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Q20 | SYSTEMS DISPLAY
In general, when are the system pages automatically displayed on the SD?
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- Relative to the current phase of flight, or
- When a system malfunction is detected
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Q21 | SYSTEMS DISPLAY
When is a STATUS page displayed?
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- After a failure is displayed on the SD and all failure items have been cleared
- STATUS will reappear when the slats are extended
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Q22 | EIS SWITCHING PANEL
What computers feed data to the six display units?
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3 Display Management Computers (DMC)
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Q23 | EIS SWITCHING PANEL
What does each of the DMCs normally supply?
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- DMC 1 – Captain PFD, ND, upper ECAM DU, lower DU
- DMC 2 – F/O PFD, ND
- DMC 3 – Backup
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Q24 | EIS SWITCHING PANEL
How can you tell if a DMC has failed?
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“INVALID DATA” will be displayed in the respective EFIS/ECAM display units
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Q25 | EIS SWITCHING PANEL
What happens when the upper ECAM display fails?
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The E/WD automatically replaces the SD on the lower ECAM display
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Q26 | EIS SWITCHING PANEL
If both the E/WD and SD display units fail, how can you display E/WD information?
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Select the ECAM/ND switch to CAPT or F/O to transfer the E/WD to either ND
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Q27 | ECAM CONTROL PANEL
With the E/WD displayed on the lower screen, how else can you view SD information?
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Press and hold the appropriate system button on the ECAM Control Panel that you wish to view
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Q28 | ECAM CONTROL PANEL
What does the ALL pushbutton do?
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- Displays ALL the system pages successively in 1-second intervals when held down
- Release the pushbutton to maintain display of the selected page
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Q29 | ECAM CONTROL PANEL
What does pressing the RCL pushbutton do?
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- Allows you to recall any warning or caution messages that the activation of the CLR pushbutton or flight phase inhibition may have suppressed
- If held longer than 3 seconds, the E/WD will show any caution messages suppressed by the EMER CANC pushbutton
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Q30 | ECAM CONTROL PANEL
If you press the STS pushbutton and the system has no STATUS messages what will be displayed?
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“NORMAL” for 5 seconds
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Q31 | ECAM CONTROL PANEL
If power fails to the ECAM CONTROL panel which buttons are still functional?
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- EMER CANC
- ALL
- CLR
- STS
- RCL
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Q32 | ECAM CONTROL PANEL
What does the EMER CANC do?
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- Cancels the current Level 1 or 2 warning for the remainder of the flight
- Cancels the current Level 3 warning for that occurrence
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Q33 | ECAM CONTROL PANEL
What do you look for on the PRELIMINARY COCKPIT PREPARATION quantity check?
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- ENG – oil quantity above 9.5 quarts + 0.5 quarts per planned flight hours
- HYD – hydraulic quantity indexes in normal filling range box (normal range + one half the normal range)
- DOOR – oxygen pressure - if half boxed in amber, check the MIN FLT CREW OXY CHART
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Q34 | ECAM CONTROL PANEL
What occurs when the T.O. CONFIG pushbutton is pressed?
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- The system simulates the application of T.O. power and checks certain systems for proper configuration
- A warning is displayed if a system is not configured properly
- “TO CONFIG NORMAL” is displayed in the TO MEMO section if the configuration is correct
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