Airbus A320
INDICATING & RECORDING
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1. The
Flight Warning Computers (FWCs) acquire data from sensors or systems to:
·
Generate
alert messages, memos, aural alerts, red warnings and synthetic voice messages,
·
Generate
Amber cautions through SDACs
·
Generate
radio altitude call-outs, DH call-outs.
·
All of the above are correct.
2. What
is the function of the System Data Acquisition Concentrators (SDACs)?
·
To
generate all visual and aural warnings.
·
To supply information to the FWCs for
warning calculations and data to the DMCs to generate displays of system pages.
·
To
generate displays of system pages to be sent to the system display unit.
3. If RA No. 1 fails, what are the degradations
·
RA flag on Capt. PFD
·
FAULT light on
GPWS SYS switch; CAT 3, GPWS in INOP of STATUS page
·
Loss of Radio Alt. Indication of Capt. PFD
·
All the above
4. For TURBULENCE detection on Wx Radar
·
Select Wx/T mode on controller
·
As in (a) and range selector should be in 40 NM or less
·
As in (b) and turbulence is
shown in magenta colour
·
None of the above
are correct
5. How can Master warning and CRC be cancelled
·
By pressing Master Warning light only
·
By pressing EMER CANC pb
·
By pressing Master Caution light
·
d Both (a) and (b) are correct.
6. When should the fast alignment of ADIRUs be done
·
During every transit stops
·
If transit time is
more than 1 hour
·
During transit
stops, if residual ground speed is more than 5 knots
·
If ADIRUs are
switched for less than one hour
7. What
does a pulsing green engine parameter indicate?
·
An ADVISORY, the parameter is about to
reach the limit.
·
An
ADVISORY, the parameter is out of the limits
·
A
MEMO, the parameter has a faulty indication.
·
A
level 3 failure requiring immediate crew action.
8. On
a bottom of the STATUS page, what does the green arrow mean?
·
It
is a reminder to land as soons as possible.
·
It
indicates that there is a system page behind.
·
It means that there is more information
to be seen.
9. The
Glide slope index will flash continuously when the deviation exceeds ______ above
______
·
1/2
dot below 120 feet RA
·
1 dot above 100 feet RA
·
1
dot above 60 ft RA
·
1/2
dot below 100 feet RA.
10. Both
LOC and glideslope will flash if, after capture, the signal is lost.
·
True.
·
False.
11. The
lower end of a red and black strip along the speed scale defines the VMAX
speed.
·
It is the lowest of the following VMO
(or MMO), VLE, VFE
·
It
is the speed corresponding to the stall warning (VSW)
·
It
represents the speed corresponding to the angle of attack at which alpha
protection becomes active.
12. The
SD displays the Gross Weight (GW) in green as soon as the second engine is
started.
·
True.
·
False.
·
Manually
·
Automatically
·
Either
manually or automatically
·
The
PFD image cannot be displayed on the ND.
14. What
is the basic role of the DMCs:
·
They compute and elaborate displays
·
Generation
of audio warnings
·
Generation
of amber warnings
·
Generation
of synthetic voice messages
15. When
should the EMER CANC push button be used?
·
At
the completion of an ECAM procedure for an abnormal procedure.
·
Whenever
a LEVEL 3 warning or LEVEL 2 caution occurs.
·
Whenever a repetitive visual or aural
warning, or caution is received that the crew has determined to be false.
16. The
actual speed is indicated by the ______ reference line.
·
yellow
·
amber
·
red
·
white
17. If
a PFD fails, does anything happen automatically?
·
The
ATT HDG switch must be used on the switching panel in order to recover PFD
information.
·
The image automatically transfers to
the display formerly occupied by the ND.
·
The
image automatically transfers to the UPPER ECAM.
·
It
has to be manually activated.
18. Course
information from the #1 ILS receiver will be displayed:
·
On the captain's PFD when the captain's
ILS push button is selected ON.
·
On
the FO's PFD when his ILS push button is selected on and on the captain's ND,
when the captain's ND is selected to ILS ROSE.
·
On
the captain's PFD and ND when the captain's ILS push button is selected ON.
·
The
first two statements are correct.
19. Information
from the #1 VOR receiver will be displayed:
·
On
the capt's PFD when the captain's VOR bearing selector is selected to VOR.
·
On the capt 's ND when the capt 's VOR
bearing selector is selected to VOR.
·
VOR
#1 course information is available on the captain's PFD and ND when the
captain's ILS pb is selected ON.
20. What
causes a display unit (DU) to go blank?
·
Loss
of power.
·
Display
unit internal failure.
·
Both are correct.
21. What
causes a DU to display a black screen with a white diagonal line?
·
DMC failure.
·
No
power.
·
Both
are correct.
22. The
maximum speed to select next higher flap setting is indicated by two amber
dashes.
·
True.
·
False
23. VOR,
ILS, and NDB raw data information is displayed on the ND in which of the
following modes?
·
VOR,
RMI and NDB information may be displayed in the ARC or ROSE NAV modes.
·
VOR
and ILS information can be displayed in the ROSE VOR and ROSE ILS modes
respectively
·
Both are correct.
24. The
presence of VOR1 in red on the ND indicates:
·
The
VOR station currently tuned is out of range.
·
The
VOR station currently tuned is out of service.
·
The # 1 VOR receiver is inoperative.
·
The
VOR station currently tuned is out of range.
25. What
is the meaning of "9000" in blue at the top of the altitude scale?
·
It marks the FCU selected altitude.
·
It
marks the airfield elevation.
·
It
marks the transition altitude.
·
It
marks the decision height.
26. How
many DMC's are there?
·
1
·
2
·
3
·
4
27. After
a single DMC failure, how could a crew member recover the display units?
·
It
is done automatically.
·
Once
a DMC has failed, the information is unrecoverable.
·
Rotate the EIS DMC switch on the
switching panel to replace the failed DMC with DMC #3.
28. Where
is information displayed by DMC #1 and DMC#2?
·
DMC#1
supplies data to PFD#1, ND#1, and lower ECAM. DMC #2 supplies data to PFD#2,
ND#2, and upper ECAM.
·
DMC#1
supplies data to PFD#1, PFD#2, and upper ECAM. DMC #2 supplies data to ND#1,
ND#2, and lower ECAM.
·
DMC#1 supplies data to PFD#1, ND#1, and
upper ECAM. DMC #2 supplies data to PFD#2, ND#2, and lower ECAM.
·
DMC#1
supplies data to PFD#1, ND#2, and lower ECAM. DMC #2 supplies data to PFD#2,
ND#1, and upper ECAM.
29. If
the lower ECAM DU fails, is there a way to retrieve that information?
·
By
pressing and holding the related systems page push button on the ECAM control
panel, the page will be displayed on the UPPER ECAM.
·
By
rotating the ECAM/ND XFR switch on the switching panel, the lower ECAM page
will be transferred to either the Captain or FO's ND.
·
Both are correct.
30. If
the UPPER ECAM DU fails, what will be displayed on the lower unit?
·
System
display page.
·
Engines and Warning page (E/WD)
·
Status
page.
31. Weather
radar can be displayed in what modes on the ND?
·
ARC
and ROSE NAV modes only.
·
ROSE
VOR and ROSE ILS modes.
·
All modes except plan.
32. How
are the FMAs displayed on the PFD?
·
There are 5 columns and 3 rows.
·
There
are 3 columns and 5 rows.
·
There
are 3 columns and 2 rows.
·
There
are 4 columns and 2 rows.
33. In
case of a double FWC failure master caution light, master warning light, aural
warnings and ECAM cautions and warnings are lost.
·
True.
·
False.
34. How
did the PNF cancel the caution for the NAV ILS 1 FAULT before calling the
STATUS page on the ECP?
·
By pressing the EMER CANC pushbutton.
·
By
pressing the CLR key
·
By
pressing the STS key
·
By
pressing the ALL key.
35. How
can the ILS 1 FAULT be restored from being a CANCELLED CAUTION?
·
By
resetting the appropriate circuit breaker.
·
By
pressing and holding any CLR key for more than 3 seconds.
·
By
pressing the EMER CAN pushbuttton for more than 3 seconds.
·
By pressing and holding the RCL key for
more than 3 seconds.
36. VLS
is the lowest speed that the autoflight system (autopilot or A/THR) will fly
the aircraft. This is a dynamic speed corresponding to an Angle Of Attack
(AOA).
·
VLS
will change with wing configuration change.
·
With
speedbrake extension, VLS will increase
·
Above
FL200, VLS will provide a 0.2g buffet margin
·
All of the above.
37. The
Speed Trend Arrow is a dynamic information displaying the speed t which the
aircraft will be in _____ .
·
5
seconds.
·
8
seconds
·
10 seconds
·
13
seconds.
38. Of
the three types of EIS displays, which one has the lowest priority?
·
The ND
·
The
PFD
·
The
SED
39. As
you approach a selected altitude, when will the yellow altitude window start
flashing?
·
As you approach within 750 ft of FCU
selected altitude and stop when it is within 250 ft.
·
As
you approach within 1000 ft of FCU selected altitude and stop when it is within
150 ft.
·
As
you approach within 500 ft of FCU selected altitude and stop when it is within
150 ft.
·
As
you approach within 900 ft of FCU selected altitude and stop when it is within
200 ft.
40. The
Flight Path vector (FPV) represents the lateral and vertical trajectory of the
aircraft with respect to the ground. On the lateral scale, it indicates the
aircraft's track. On the vertical scale, it indicates the aircraft's flight
path angle.
·
True.
·
False.
41. When
does the Side Stick Order indicator display?
·
After
first engine start and disappears when passing 400 feet RA
·
After first engine start and disappears
after rotation
·
After
seconde engine start and disappears when passing 400 feet RA
·
After
second engine start and disappears when passing 400 feet RA
42. When
is the 'Green Dot' displayed?
·
Only when flap handle is the zero position.
·
Only
when flap handle is the zero position, above FL80
·
Only
when flap handle is the zero position, below FL80
·
Only
when flap handle is the zero position, below FL85
43. What
does Green Dot represent?
·
Maneuvering
speed in clean configuration
·
Maneuvering speed in clean
configuration when speed is managed.
·
The
next flap extend (VFE) max speed
·
The
flap extend min speed from clean configuration
44. The
green 'S' of the speed tape is the Minimum Slat Retraction Speed. It is only
displayed when the flap handle position is in position 1.
·
True.
·
False.
45. When
will the PFD Heading tape revert to TRU heading?
·
North of 73° North or South of 60°
South
·
South
of 73° North or North of 60° South.
·
North
of 80° North or South of 73°South
·
North
of 78° North or South of 78°South
46. Is
the Side Slip indicator always yellow?
·
Yes.
·
No, it turns blue when it becomes a
beta target (displaying optimum side slip for a given configuration)
·
No,
it turns orange when it becomes a beta target .
47. When
will the Flight Directors bars flash?
·
When
a reversion occurs.
·
When
loss of LOC or G/S signal in LAND mode.
·
All of the above.
48. The
Flight Director bars are out of view when Bank angle exceeds 67°.
·
True
·
False.
49. If
the FPV (Flight Path Vector) symbol is right of center, where is the wind
coming from?
·
Right.
·
Left.
·
It
depends of the Track followed
50. If
the FPV is above the horizon line, what is the aircraft actually doing?
·
Descending.
·
Maintaining
FL.
·
Climbing.
·
Cannot
say.
51. Do
the Check ATT. Messages appear on both PFDs at the same time?
·
Yes
·
No
·
Message
only appears on the EWD
·
Message
only appears on ECAM
52. FACs
calculate speed trend and VLS. The extremities of the trend vector and V1s
segment indicate respectively; speed value at the next 10 seconds and 1.23 Vs 1
g with present configuration. Is this correct?
·
Yes (for both cases)
·
No
(for both cases)
·
No
because VLS is not 1.23 Vs 1g
·
No
because the tip of the speed arrow is not the speed in 10 seconds time
53. With
radar selected on, what can you read on ND about antenna setting?
·
Tilt
angle
·
Tilt angle and gain mode
·
Roll
angle and tilt angle
·
Nothing
54. RNAV
position information is displayed on the ND in which of the following modes?
·
ARC and ROSE NAV modes only.
·
ROSE
VOR and ROSE ILS modes.
·
ARC,
ROSE and PLAN modes.
·
ROSE
VOR mode.
55. Once
the crewmember has completed viewing a specific system, what is the correct
procedure for clearing the screen and returning it to a normal presentation?
·
Press the respective system push button
again.
·
It
goes away by itself.
·
Press
CLR on the ECAM control panel.
·
Press
twice CLR on the ECAM control panel.
56. After
the engine shutdown, you observe a pulsing STS message. What does it mean?
·
It
is an indication that at least one system requires crew attention.
·
It
is an indication that the aircraft has not been shut down correctly.
·
It is a reminder that the status page
holds a maintenance message.
57. The
upper ECAM Display Unit (DU) has failed. You want to see the DOOR/OXY page. How
can you see it?
·
You have to press and hold the DOOR key
on the ECP.
·
You
have to switch the EIS DMC to CAPT3
·
You
have to press and hold the RCL key on the ECP.
58. Both
ECAM screens have failed. Is it possible to get E/WD indications?
·
Yes,
the E/WD is automatically transferred to one of the NDs.
·
No.
The E/WD is lost until the aircraft can be repaired.
·
Yes, to get E/WD information. It must
be manually transferred to one of the NDs.
·
Yes.
E/WD information is automatically transferred to the the F/O's PFD in the event
of an ECAM warning.
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