SH Chapter 10 - Flight Instruments & Displays Flashcards

1
Q

1) What do the large red arrowheads on the PFD indicate?

A

Direction to move the nose to reduce pitch (occurs beyond 30 degrees nose up or down)

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2
Q

2) What are the pitch and roll protection limits indicated by the green = signs?

A

30 degrees NU, 15 degrees ND, and 67 degrees roll

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3
Q

3) When would the sideslip index change from yellow to blue?

A

Engine failure at take off or go around

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4
Q

4) What does the yellow speed trend pointer on the airspeed display indicate?

A

Where this speed will be in 10 seconds if acceleration remains constant

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5
Q

5) What is the difference between the magenta and blue target airspeeds?

A

Magenta is managed and blue is selected

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6
Q

6) What is Vls and how is it displayed?

A

Lowest selectable airspeed (lowest speed providing adequate margin to stall speed). Amber line on ASI.

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7
Q

7) What speed does VMAX represent and how is it displayed?

A

Lowest if Vmo, Mmo, Vle or Vfe.

Displayed by lower end of red and black strip on ASI

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8
Q

8) What is Green Dot speed?

A

Engine out clean speed (equates to best L/D speed)

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9
Q

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

A

Aircraft has deviated from FCU selected altitude or FL by 250 feet.

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10
Q

10) When is altitude alerting and the C chord automatically inhibited in flight?

A

Altitude Alerting
Slats are out with gear down, in approach after glide slope capture and gear down and locked.
C Chord
When AP on and approaching a selected altitude or FL

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11
Q

11) What does it mean when the altitude digits change from green to amber on the PFD

A

On approach, for which a minimum has been entered into FMGS, if the aircraft goes below minimum

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12
Q

12) When is Radio Height displayed on the PFD?

A

Below 2500’ AGL.

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13
Q

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

A

When approach mode has been armed but LS pb has not been selected

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14
Q

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

A

White if DES not armed. Blue if DES armed.

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15
Q

15) What color does each altitude constraint circle on the ND represent?

A

Magenta when ALT CSTR is predicted to be met. Amber when predicted to be missed, and white when not taken into account by FMGS & NAV mode armed

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16
Q

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

A

?

Default selection is ROSE NAV and 80NM

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17
Q

17) What are the 3 levels of ECAM Failure Mode Notifications?

A

Level 3 - Red Warning
- Immediate action
- CRC, master warning, red warnings & SD auto displays
Level 2 - Amber Caution
- System failure without any direct consequence to safety
- Single chime, master caution & SD auto displays (some exceptions)
Level 1 - Amber Caution
- Failures leading to loss of redundancy or system degradation
- No aurals, caution message on upper ECAM without procedure

18
Q

18) If simultaneous failures occur, how will they be presented to the crew on the ECAM?

A

Priority for failures are level 3 first, then level 2, then level 1

19
Q

19) What categories of failures are presented to the crew on the EWD?

A

Independent- Failure that affects isolated system or item
Primary - Failure that costs use of other system
Secondary - Loss of system from primary failure

20
Q

20) What indication does the EWD provide for secondary failures?

A

“*” in front

21
Q

21) What does the appearance of a green arrow at the bottom of the EWD screen indicate?

A

Too many messages for the space available

22
Q

22) What does the display of TO INHIBIT or LDG INHIBIT indicate?

A

During high workload times, some warnings and cautions are being inhibited

23
Q

23) When does the Takeoff Memo appear on the EWD?

A

Either 2 mins after second engine started or when TO CONFIG test button is pressed with one engine running

24
Q

24) When does the Landing Memo appear EWD?

A

Below 2000’ (goes away after touchdown below 80 kts)

25
Q

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

A

Displays page related to the present flight phase (unless system malfunction or other mode engaged)

26
Q

26) When is a STATUS page displayed?

A

When crew presses STS on ECAM Control Panel
Automatically in abnormal operations if crew clears last alert, and STATUS not empty or if crew selects CONFIG 1 and status page not empty

27
Q

27) What computers feed data to the six display units?

A

Three Display Management Computers (DMCs)

28
Q

28) Explain how each DMC normally supplies the different display units?

A

DMC 1 - Drives Capt PFD, ND and ECAM
DMC 2 - Drives FO PFD & ND
DMC 3 - On standby

29
Q

29) How can you tell if a DMC has failed?

A

INVALID DATA displayed on Display Unit

30
Q

30) What happens when the upper ECAM display fails?

A

Automatically switches to lower ECAM

31
Q

31) If both the EWD and SD display units fail, how can you display EWD information?

A

Use the ECAM/ND XFR knob and push and hold the related system page. Then displayed on Capt or FO ND, whichever was selected.

32
Q

32) With the upper EWD displayed on the lower screen, how else can you view SD information?

A

Use the ECAM/ND XFR knob or push and hold the related system page pb and it will be displayed on lower ECAM

33
Q

33) What does pressing the ALL pb on the ECAM control panel accomplish?

A

Displays all system pages at 3 second intervals

34
Q

34) What does pressing the RCL pb on the ECAM control panel do?

A

Displays all alters previously cleared by CLR pb that are still active.
If you hold for more than 3 seconds, displays all alerts previously cleared and all alerts cancelled via EMER CANC pb.

35
Q

35) If you press the STS pb and the system has no STATUS messages, what will be displayed?

A

“NORMAL” for 3 seconds

36
Q

36) If power fails to the ECAM control panel, which buttons are still functional?

A

CLR, RCL, STS, EMER CANC & ALL pbs remain operative.

37
Q

37) What does the EMER CANC pb do when a warning exists?

A

Silences the aural warning and clears MASTER WARN but doesn’t affect the ECAM messages.
For cautions it cancels any present caution for the rest of the flight.

38
Q

38) What occurs when the T.O CONFIG pb is pressed?

A

Simulates application of TO power.

Test that triggers a warning if the aircraft is not in take off configuration.

39
Q

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

A

On ground during first 5 mins of aircraft power up, or after first engine start and in flight. Stops automatically 5 mins after second engine shutdown.

40
Q

40) What is the purpose of the DFDR EVENT pb?

A

Sets an event marker on FDR records.