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Frontier Study Guide > CPT Written Test > Flashcards

CPT Written Test Flashcards

1
Q

The temperature of each aircraft zone is optimized by what means

A

A trim air valve

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2
Q

Under what condition should the pack flow selector be set to LO?

A

With a low passenger load to reduce bleed air demand and improve fuel efficiency

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3
Q

The pack flow selector is set to NORM and yet the ECAM display shows pack flow to be high.
How is this possible?

A

HI flow is automatically selected regardless of PACK FLOW select position because air is only being supplied by the APU.

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4
Q

What does the safety valve protect against?

A

Cabin differential pressure from going too high or too low.

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5
Q

Having manually sent the LDG ELEV, the cabin altitude is:

A

Still controlled automatically through the outflow valve.

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6
Q

The safety valves are

A

Fully automatic and cannot be controlled manually.

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7
Q

By moving the MAN V/S CTL to this position

A

The cabin altitude is raised by opening the outflow valve

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8
Q

Which ECAM key would you choose to access the ventilation information?

A

PRESS

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9
Q

With both the BLOWER and EXTRACT pb switches in OVRD, what happens to the ventilation system?

A

The system goes to smoke configuration and the blower fan stops.

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10
Q

The blue LOC is in armed mode

A

True

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11
Q

A/THR in white mode means it is?

A

Active

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12
Q

The thrust delivered by a/THR is already to MAX CLB thrust. Is it possible to obtain some additional thrust?

A

Yes, by moving the thrust levels forward to the CL detent.

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13
Q

According to this display:

A

The speed is managed by the FM

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14
Q

During the takeoff phase:

A

SRS mode will provide guidance to maintain V2 + 10KTS (minimum) as a speed reference up to the acceleration altitude

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15
Q

According to this FMA:

A

The A/THR is off, the aircraft is on the localizer and the G/S is armed

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16
Q

How can you get the mechanics attention when he is outside the aircraft?

A

Use the MECH pb switches on the CALLS panel, which sounds an external horn

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17
Q

During preflight, you have to check the CVR. The parking brake is on. How would you begin this test?

A

A

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18
Q

How do you erase the CVR?

A

Press, the CVR ERASE pb when the aircraft is on the ground with the parking brake set.

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19
Q

With the AUDIO SWITCH knob in the CAPT 3 position, the captain uses his acoustic equipment on ACP 3

A

True

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20
Q

You enter a dark cockpit, what action is necessary before checking the battery voltage

A

You have to check that both batteries are set to off

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21
Q

According to these indications, which statement is true

A

Both battery voltages are above the minimum of 25.5 V

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22
Q

If the battery voltages are below the minimum, how do you charge them?

A

I have to check that the BAT pb are on and switch the external power on

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23
Q

After having switched the external power to ON, you get the following indications. What do they mean?

A

On the ground, these indications are normal when the engines are not running

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24
Q

Take a look at the ECAM. Now that the IDG oil temperature has cooled, the IDG can be reconnected by pressing the IDG push button.

A

False

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25
A master warning and caution has come on. You notice the red FAULT light on the EMER ELEC PWR panel. How do you interpret this indication?
The EMER GEN is not yet supplying the system
26
You want to open the cabin door. While lifting the control handle, the white light comes on. What does this mean?
The slide is still armed
27
With the EMER GEN online, how would you expect the ELEC page to look?
C
28
There is no way to deploy the over wing escape slide if it fails to deploy automatically after opening the emergency exit
False
29
In this given situation, if somebody opens the left door from the outside, the slide will not deploy
True
30
If the oxygen masks fail to deploy automatically they:
Can be deployed by pressing the MASK MAN ON pb on the overhead panel.
31
Can the APUFIRE test be done using battery power only
Yes
32
While carrying out the APU FIRE test on battery power only you see the indications at the right, is the test successful
Yes
33
According to the indications at right
One fire detection loop for engine one has failed. Fire detection for both engines is still available.
34
With reference to cargo compartment, fire extinguishing with two fire bottles, which statement is true?
Both B and C
35
How many actuators are provided to control the rods and how many hydraulic sources supply these actuators?
A; 2 hydraulic, 4 actuators
36
The message WING TIP BRK ON appears on the E/WD. What does it mean?
The hydraulic device locks the flaps in their present position
37
Are there any control services with a mechanical backup?
Yes, the THS and rudder
38
Give the scenario displayed at right? What will happen next
The left spoiler 3 will be retracted, the right spoiler 3 will be inhibited to prevent asymmetry
39
In normal law, if one side stick is rapidly pulled full back, can the aircraft maximum allowable “G” load be exceeded
No, the load factor, limitation overrides sidestick commands to avoid excessive “G” loads
40
According to the indications at right, if you release the sidestick now
The bank angle will automatically return to 33°
41
In normal law, what is the maximum bank angle you can reach with the side stick fully deflected
67°
42
According to the indications at right which flight control law is active?
Direct
43
According to the indications at right
No protection is triggered
44
According to the indications at right
The Alpha floor protection has automatically set TOGA thrust
45
According to the display at right, which statement is correct
All the pumps are on, but no fuel is being used
46
What does the message CTR TK FEEDG mean at right
The fuel quantity indication is inaccurate
47
After engine shut down, what are your actions to close the fuel transfer valves?
No action is required. The valves will close automatically during the next refueling
48
How has the fuel been transferred from the outer to the inner tanks?
The transfer valves have been opened automatically by the low level sensor in the inner tank
49
Why do the center tank pumps stop automatically when the slats are extended for takeoff?
To ensure that the engines are fed from the wing tanks for takeoff
50
What is the minimum fuel quantity for takeoff?
3300 LBS
51
In the situation depicted, the right inner tank fuel is unavailable for the rest of the flight
False
52
You have not started the engines, but the cargo door is being operated, which HYD page at right depicts this
C
53
To power the BLUE hydraulic system with the rat can be deployed
By lifting the cover and pushing RAT MAN ON pb
54
Which is the correct indication at right when the RAT is powering the BLUE system
D
55
What is the normal pressure in the hydraulic system?
3000 psi
56
During start up when is the blue hydraulic system pressurized
Automatically after the first engine start
57
Which statement below is correct
The PTU enables the green and yellow systems to pressurize each other when the differential pressure is greater than 500 psi
58
Which key on the ECAM control panel should be pressed to get information about the anti-ice system?
A. (Bleed).
59
What is the normal indication on the bleed page at right given the anti-ice panel selection below
D
60
Give the indications on the right
The left wing anti-ice valve has failed to close
61
With reference to the PROBE/WINDOW HEAT pb, which of the following statements is true
D. Window heating comes on automatically after first engine start
62
If one engine anti-ice system fails. The second one takes over and provides anti-ice for both engines.
False
63
In the event of an electrical power supply loss
The engine anti-ice valves will open automatically
64
Which cam memo display would you expect to see with the anti-ice selection below?
C
65
What is the maximum speed limit for operating the windshield wipers?
The 230 KTS
66
Which color coating on the EFIS screens indicates that crew awareness is required
B
67
What does a posting green indication mean on the SD?
A. An ADVISORY, the parameter is about to reach a limit
68
What does the green arrow at the bottom of the STATS page at right indicate:
It means that there is more STATUS information to be seen
69
The upper display unit (DU) has failed. You want to see the DOOR/OXY page on the lower DU, how would you do this?
Press and hold the DOOR key on the ECP
70
The upper display unit has failed. How would you get the ECAM system pages to appear on the CA‘s ND
D. Move the ECAM/ND XFR to CAPT
71
Which key on the ECP was pressed to cancel the NAV ILS 2 fault?
B.
72
What is wrong with the FO‘s EFIS in the display at right?
C. The FD should be on.
73
What is the maximum speed to further extend the flaps as displayed at right?
C. 175kts
74
What is the meaning of the 9000 in blue at the top of the altitude scale displayed at right?
A. It is the FCU selected altitude.
75
Which of the following statements is correct regarding the display at right?
D. The track to PAS is 108° and the estimated time crossing PAS is 1430Z.
76
What does the NWSTRGDISC memo at right mean
A. The nose wheel steering has been disconnected by the ground crew.
77
You are ready to TAXI and apply pedal brakes to release the parking brake the brakes pressure fall to 0.
B. This is normal; the indicator only displays alternate (Yellow) brake pressure.
78
There are two triangles for each gear on the ECAM WHEEL page; what do they represent?
B. Each triangle represents the year position detected by one of the 2 LGCIUs
79
How do you interpret the indications at right?
B. All gear are down and locked as detected by LGCIU 2. One green gear triangle indication is enough to confirm that the gear is down and locked.
80
How do you interpret the green arc shown over wheel 2 at right?
A. It indicates the hottest break with the temperature greater than 100°C
81
What triggers the AUTO/BRK operation in MED after landing
B. Ground spoiler extension after a short delay.
82
Which indication confirms that the control of the oxygen mask doors has been activated
B.
83
With the oxygen crew supply switch off, which ECAM indication would you see?
A.
84
During the automatic start sequence of ENG 2, you noticed that the igniter B is powered. Is it normal?
D. Yes, igniters are used alternately for engine start.
85
After takeoff the A/THR will not become active until
A. The thrust levels are placed in the CLIMB position
86
You are at the start of a decent and a green N1 arc is displayed showing the new thrust demand. When does this happen?
D. Whenever there is a power change with auto thrust engaged.
87
A few seconds after selecting reverse, the amber RTV indication changes to green. What does this mean?
B. The reverses are now fully deployed
88
During engine start the Amber FAULT light on the ENG MASTER panel comes on. This indicates.
A. The automatic start sequence has been aborted.
89
During a manual start, what function does the FADEC carry out?
A. Passive monitoring of the start sequence, to close the start valve and cut off the ignition on the ground.
90
You are in the middle of a manual engine start. What are you looking for when you select ENG MASTER 2 ON?
C. The fuel used is reset, both igniters are powered and fuel flow is indicated.
91
During ground maneuvering, what part of the A321 aircraft is the obstacle clearance constraint?
C. Tail.
92
When the A321 ECON FLOW pb is ON the airflow is 80% of normal but will automatically increase to 100% if the temperature demand requires more airflow with single pack operation or with the AP supply and bleed air 120% of normal flow will be provided
True

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