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Allegiant A320 Systems (2024) > Indicating & Recording > Flashcards

Indicating & Recording Flashcards

1
Q

Q1 | RECORDER PANEL

When does the Digital Flight Data Recorder (DFDR) operate?

[ FCOM-DSC-31-60-10 ]

A
  • 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

[ FCOM-DSC-31-60-10 ]

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2
Q

Q2 | RECORDER PANEL

What is the purpose of the DFDR EVENT pushbutton?

[ FCOM-DSC-31-60-20 ]

A

Briefly pressing this button sets an event mark on the Flight Data Recorder

[ FCOM-DSC-31-60-20 ]

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3
Q

Q3 | RECORDER PANEL

What would be indicated if the altitude window changed from yellow to amber?

[ FCOM-DSC-31-40 ]

A

The aircraft has deviated from the FCU selected altitude or flight level by 250 feet

[ FCOM-DSC-31-40 ]

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4
Q

Q4 | RECORDER PANEL

When is altitude alerting automatically inhibited in flight?

[ FCOM-DSC-31-40 ]

A
  • When slats are extended with the landing gear selected down
  • On approach after glide slope capture
  • When the landing gear is locked down

[ FCOM-DSC-31-40 ]

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5
Q

Q5 | RECORDER PANEL

What does it mean when the altitude digits change from green to amber?

[ FCOM-DSC-31-40 ]

A

The aircraft has descended below the MDA/DH entered into the FMGC

[ FCOM-DSC-31-40 ]

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6
Q

Q6 | RECORDER PANEL

When is Radio Height displayed on the PFD?

[ FCOM-DSC-31-40 ]

A

Below 2,500 feet AGL

[ FCOM-DSC-31-40 ]

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7
Q

Q7 | RECORDER PANEL

What would a flashing amber ILS indicate on the bottom of the PFD?

[ FCOM-DSC-31-40 ]

A

Flashes amber when APPR mode is armed and the LS display is not selected

[ FCOM-DSC-31-40 ]

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8
Q

Q8 | RECORDER PANEL

Information from ILS receiver 1 is displayed where?

[ FCOM-DSC-34-30-20 ]

A
  • Captain’s PFD
  • F/O’s ND

[ FCOM-DSC-34-30-20 ]

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9
Q

Q9 | NAVIGATION DISPLAY

Top of Descent and Continue Descent arrows are displayed in blue or white. What is the difference?

[ FCOM-DSC-31-45 ]

A
  • Top of Descent – Always white (never armed)
  • Continue Descent – Blue indicates armed, white indicates NOT armed

[ FCOM-DSC-31-45 ]

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10
Q

Q10 | NAVIGATION DISPLAY

What color does each altitude constraint circle represent?

[ FCOM-DSC-31-45 ]

A
  • White – constraint is not taken into account
  • Magenta – constraint is predicted to be satisfied
  • Amber – constraint is predicted to be missed

[ FCOM-DSC-31-45 ]

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11
Q

Q11 | NAVIGATION DISPLAY

If mode range data fails what should you expect to see on the ND?

[ FCOM-DSC-31-50 ]

A

ROSE NAV mode at 80 nm range

[ FCOM-DSC-31-50 ]

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12
Q

Q12 | ENGINE WARNING DISPLAY

What are the 3 levels of ECAM Failure Mode Notifications?

[ FCOM-DSC-31-10 ]

A
  • Level 1 – ALERT:
    • Associated with amber E/WD message, no aural signal, and requires crew monitoring
  • Level 2 – CAUTION:
    • Associated with the amber MASTER CAUT light, single chime, and require crew awareness
  • Level 3 – WARNING:
    • Associated with the red MASTER WARN light, CRC, and require immediate action

[ FCOM-DSC-31-10 ]

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13
Q

Q13 | ENGINE WARNING DISPLAY

If simultaneous failures occur, how will they be presented to the crew?

[ FCOM-DSC-31-10 ]

A

A level 3 Warning has priority over a level 2 Caution which has priority over a level 1 Alert

[ FCOM-DSC-31-10 ]

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14
Q

Q14 | ENGINE WARNING DISPLAY

What types of failures are presented to the crew?

[ FCOM-DSC-31-10 ]

IPS

A
  • 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

[ FCOM-DSC-31-10 ]

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15
Q

Q15 | ENGINE WARNING DISPLAY

What indication does the E/WD provide for secondary failures?

[ FCOM-DSC-31-15 ]

A

Secondary failures are displayed on the lower right portion of the E/WD and are preceded by an *

[ FCOM-DSC-31-15 ]

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16
Q

Q16 | ENGINE WARNING DISPLAY

What does the appearance of a green arrow at the bottom of the E/WD screen indicate?

[ FCOM-DSC-31-15 ]

A

Information has overflowed off the screen and the pilot must scroll down using the CLR pushbutton on the ECAM panel

[ FCOM-DSC-31-15 ]

17
Q

Q17 | ENGINE WARNING DISPLAY

What does the display of T.O. INHIBIT or LDG INHIBIT indicate?

[ FCOM-DSC-31-15 ]

A

Most warnings and cautions are inhibited to avoid unnecessary distractions during critical phases of flight

[ FCOM-DSC-31-15 ]

18
Q

Q18 | ENGINE WARNING DISPLAY

When does the Takeoff Memo appear?

[ FCOM-DSC-31-15 ]

A
  • 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

[ FCOM-DSC-31-15 ]

19
Q

Q19 | ENGINE WARNING DISPLAY

When does the Landing Memo appear?

[ FCOM-DSC-31-15 ]

A
  • Below 2,000 feet RA
  • Memo disappears after touchdown (80 knots)
  • Displays at 800 feet if you never climbed above 2000 feet RA

[ FCOM-DSC-31-15 ]

20
Q

Q20 | SYSTEMS DISPLAY

In general, when are the system pages automatically displayed on the SD?

[ FCOM-DSC-31-20 ]

A
  • Relative to the current phase of flight, or
  • When a system malfunction is detected

[ FCOM-DSC-31-20 ]

21
Q

Q21 | SYSTEMS DISPLAY

When is a STATUS page displayed?

[ FCOM-DSC-31-20 ]

A
  • After a failure is displayed on the SD and all failure items have been cleared
  • STATUS will reappear when the slats are extended

[ FCOM-DSC-31-20 ]

22
Q

Q22 | EIS SWITCHING PANEL

What computers feed data to the six display units?

[ FCOM-DSC-31-05-10 ]

A

3 Display Management Computers (DMC)

[ FCOM-DSC-31-05-10 ]

23
Q

Q23 | EIS SWITCHING PANEL

What does each of the DMCs normally supply?

[ FCOM-DSC-31-05-30 ]

A
  • DMC 1 – Captain PFD, ND, upper ECAM DU, lower DU
  • DMC 2 – F/O PFD, ND
  • DMC 3 – Backup

[ FCOM-DSC-31-05-30 ]

24
Q

Q24 | EIS SWITCHING PANEL

How can you tell if a DMC has failed?

[ FCOM-DSC-31-05-50 ]

A

“INVALID DATA” will be displayed in the respective EFIS/ECAM display units

[ FCOM-DSC-31-05-50 ]

25
Q

Q25 | EIS SWITCHING PANEL

What happens when the upper ECAM display fails?

[ FCOM-DSC-31-05-60 ]

A

The E/WD automatically replaces the SD on the lower ECAM display

[ FCOM-DSC-31-05-60 ]

26
Q

Q26 | EIS SWITCHING PANEL

If both the E/WD and SD display units fail, how can you display E/WD information?

[ FCOM-DSC-31-05-60 ]

A

Select the ECAM/ND switch to CAPT or F/O to transfer the E/WD to either ND

[ FCOM-DSC-31-05-60 ]

27
Q

Q27 | ECAM CONTROL PANEL

With the E/WD displayed on the lower screen, how else can you view SD information?

[ FCOM-DSC-31-05-60 ]

A

Press and hold the appropriate system button on the ECAM Control Panel that you wish to view

[ FCOM-DSC-31-05-60 ]

28
Q

Q28 | ECAM CONTROL PANEL

What does the ALL pushbutton do?

[ FCOM-DSC-31-30 ]

A
  • Displays ALL the system pages successively in 1-second intervals when held down
  • Release the pushbutton to maintain display of the selected page

[ FCOM-DSC-31-30 ]

29
Q

Q29 | ECAM CONTROL PANEL

What does pressing the RCL pushbutton do?

[ FCOM-DSC-31-30 ]

A
  • 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

[ FCOM-DSC-31-30 ]

30
Q

Q30 | ECAM CONTROL PANEL

If you press the STS pushbutton and the system has no STATUS messages what will be displayed?

[ FCOM-DSC-31-30 ]

A

“NORMAL” for 5 seconds

[ FCOM-DSC-31-30 ]

31
Q

Q31 | ECAM CONTROL PANEL

If power fails to the ECAM CONTROL panel which buttons are still functional?

[ FCOM-DSC-31-30 ]

A
  • EMER CANC
  • ALL
  • CLR
  • STS
  • RCL

[ FCOM-DSC-31-30 ]

32
Q

Q32 | ECAM CONTROL PANEL

What does the EMER CANC do?

[ FCOM-DSC-31-30 ]

A
  • Cancels the current Level 1 or 2 warning for the remainder of the flight
  • Cancels the current Level 3 warning for that occurrence

[ FCOM-DSC-31-30 ]

33
Q

Q33 | ECAM CONTROL PANEL

What do you look for on the PRELIMINARY COCKPIT PREPARATION quantity check?

[ FCOM-PRO-NOR-SOP-04 ]

A
  • 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

[ FCOM-PRO-NOR-SOP-04 ]

34
Q

Q34 | ECAM CONTROL PANEL

What occurs when the T.O. CONFIG pushbutton is pressed?

[ FCOM-DSC-31-30 ]

A
  • 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

[ FCOM-DSC-31-30 ]

Allegiant A320 Systems (2024) (18 decks)

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