問題一覧
1
The pitch direct law is:
A direct side stick to elevator relationship
2
How many degrees down do the ailerons extend (aileron drop)?
They extend 5 degree down when the flaps are extended
3
Which surfaces are used for lift dumping on ground?
All spoilers, 1 to 5
4
Which signals cause rudder pedal movement?
Rudder trim signals
5
If ELAC 1 and 2 have failed:
The elevator and pitch trim are controlled by SEC 1 or 2
6
If FAC 1 and 2 have failed:
The rudder can always be controlled from the pedals
7
When both sticks are moved in the same or opposite direction:
The surface movement is proportional to the algebraic sum of the deflections of both sticks
8
Elevators, ailerons and spoilers are:
Hydraulically activated and electrically controlled
9
Rudder control is electrical for yaw damping and trim:
Yes
10
What statement is correct:
Ground spoiler function: all spoilers deploy
11
How many control modes are there on the elevator's servo jacks?
3
12
What are the limits for maneuver protection:
Both (+2.5 G - 1 G clean) and (+2 G - 0 flaps extended) are correct
13
Which ELAC normally controls the elevators and the stabilizer:
ELAC 2
14
How many hydraulic motors drive the screw jack of the stabilizer:
2
15
How many electric motors can control the hydraulic motor of the stabilizer:
3
16
In normal law, the flight mode changes to the flare mode when passing:
50 ft
17
How can a deactivated stick be reactivated:
By momentary action on either stick take over push buttons
18
At landing when passing 30 ft:
The attitude is progressively reduced to 2° nose down, to force the pilot to make a nose up input
19
In roll normal law, the bank angle protection is active when bank angle is:
> 67°
20
The roll normal law provides combined control of the:
Ailerons + spoilers 2 to 5 + rudder
21
If ELAC 1 and ELAC 2 have failed:
Roll control is provided by spoilers only
22
In flight, if a WTB (wing tip brake) is activated, can you release it?
No
23
If configuration 0 is not selected after take-off, the flaps automatically retract at:
210 kts
24
What happens when SFCC 1 fails:
Flaps and slats operate at half speed
25
After FLAP retraction, when is CONF 1+F available again?
At 100 kt or less
26
Is it possible to select an intermediate position with the flaps and slats selector?
No
27
If you are flying at an angle of attack more than Alpha Prot, what happens when you release the stick?
Speed returns to Alpha Prot
28
When roll direct law is active, the yaw damping is:
Lost
29
Sideslip target:
To indicate how much rudder to use to get the best climb performance in case of engine failure
30
How many hydraulic systems activate the rudder:
3
31
Slat retraction from 1 to 0 is inhibited if angle of attack exceeds 8.5 degrees or speed < 148 knots:
Alpha/Speed Lock
32
In alternate law, the change to direct law occurs when:
Landing gear down or at the selection of flaps 2 (LGCIU 1 + 2 fault)
33
SLATS SYS 1 FAULT on the ECAM warning display means:
The slat channel in one SFCC has failed
34
With blue hydraulic system remaining and before landing gear extension, the flight control law is:
Alternate
35
In normal law, the stall warning is activated:
Angle of attack corresponding to stall warning can’t be reached in normal law
36
The pitch normal law provides:
Manoeuvre + high angle of attack + high speed + pitch attitude protection
37
When is the THS not available?
After yellow and green hydraulic system failure
38
Flight control computers are:
2 ELACs - 3 SECs - 2 FACs
39
When bank angle protection is active, is auto trim inoperative?
Yes
40
The PFD displays in amber the message "USE MAN PITCH TRIM" in
Direct Law
41
If neither ELAC 1 nor ELAC 2 are available, pitch control is automatically transferred to:
SEC 1 or SEC 2
42
If one Flap power control unit fails, what happens:
Flaps at half speed
43
After an automatic retraction of the flaps with CONF. 1, the flaps will automatically re-extend when speed decreases:
No
44
When ALT LAW is active, the High Speed and High Angle of Attack protections are:
Lost
45
When ALT LAW is active, the Yaw Damping is:
Available (damper authority is limited to ±5 degrees of rudder deflection)
46
When in CONF 1+F, the flaps retract to 0o automatically at 210 kts:
Automatic Retraction function
47
Lift augmentation is achieved on each wing by:
2 flap surfaces + 5 slat surfaces
48
Which flight control computer normally operates the ailerons?
Elevator and aileron computer (ELAC) 1
49
In normal law, what happens if the pilot holds full lateral side stick deflection?
The bank angle goes to 67° and no further
50
What is true regarding the flight controls on an A320?
They are all electrically controlled and hydraulically activated
51
Which spoilers are ground spoilers?
Spoilers 1-5