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