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QT A320 > ATA27 - Flight controls > Flashcards

ATA27 - Flight controls Flashcards

1
Q
  1. At landing when passing 30 ft :
    The attitude is memorized
    The attitude is progressively reduced to 2° NOSE DOWN
A

The attitude is progressively reduced to 2° NOSE DOWN

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2
Q
  1. If FAC 1 and 2 have failed :
    The RUDDER can still be controlled from the pedals
    The RUDDER CONTROL is lost
    THE RUDDER CONTROL is provided by SEC 3
A

The RUDDER can still be controlled from the pedals

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3
Q
  1. If you are flying at an angle of attack of more than ALPHA PROT what happens when
    you release the stick :
    SPEED returns to VLS
    SPEED returns to ALPHA PROT
A

SPEED returns to ALPHA PROT

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4
Q
  1. How many control modes are there on the ELEVATORS servojacks ?
    2
    3
    4
A

3

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5
Q
  1. The PITCH DIRECT LAW is :
    A load factor demand with no protection
    A direct side stick to elevator relationship
    A direct side stick to elevator relationship with AUTOTRIM operation
A

A direct side stick to elevator relationship

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6
Q
  1. Is it possible to select an intermediate position with the FLAPS and SLATS
    SELECTOR :
    Yes
    No
A

No

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7
Q
  1. SLATS SYS 1 FAULT on the ECAM WARNING DISPLAY means :
    SFCC 1 has failed
    The SLAT CHANNEL in one SFCC has failed
A

The SLAT CHANNEL in one SFCC has failed

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8
Q
  1. How can a non permanently deactivated stick be reactived :
    By releasing the TAKE OVER P/B of the active stick
    By a momentary action on TAKE OVER P/B of deactivated stick
    Both answers are correct
A

Both answers are correct

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9
Q
  1. When is the THS not available ?
    After a BLUE HYDRAULIC SYSTEM failure
    After a YELLOW and GREEN SYSTEM failure
    Never lost, always available manually
A

After a YELLOW and GREEN SYSTEM failure

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10
Q
  1. RUDDER CONTROL is electrical for RUD TRIM and RUD TRAVEL :
    Yes
    No
A

Yes

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11
Q
  1. How many HYDRAULIC MOTORS does the SCREW JACK of the STABILIZER
    DRIVE?
    2
    3
A

2

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12
Q
  1. When both sticks are moved in the same or opposite direction and neither takes
    priority :
    The surface movement is proportional to the algebraic sum of both signals
    The surface movement is proportional to the last stick deflected
    The surface movement is proportional to the first stick deflected
A

The surface movement is proportional to the algebraic sum of both signals

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13
Q
  1. In flight, if a WTB (WING TIP BRAKE) is activated, can you release in flight ?
    Yes
    No
A

No

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14
Q
  1. ELEVATORS, AILERONS and SPEED BRAKES are :
    Hydraulically activated and mechanically controlled
    Electically activated and hydraulically controlled
    Hydraulically activated and electrically controlled
A

Hydraulically activated and electrically controlled

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15
Q 
173. In ROLL NORMAL LAW, the BANK ANGLE PROTECTION is active when BANK
ANGLE is :
> 45°
> 33°
> 67°
A

> 33°

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16
Q
  1. Which ELAC NORMALLY CONTROLS the ELEVATORS and the STABILIZER :
    ELAC 1
    ELAC 2
A

ELAC 2

17
Q
  1. Which statement is correct ?
    GROUND SPOILER function : all SPOILERS deploy
    SPEED BRAKE function : SPOILERS 1, 2, 3 deploy
    ROLL function : AILERONS + SPOILERS 4 and 5 deploy
A

GROUND SPOILER function : all SPOILERS deploy

18
Q
  1. What are the limits for maneuver protection ?
    + 2,5 g to - 1 g for clean configuration
    + 2 g to 0 g FLAPS extended
    Both answers are correct
A

Both answers are correct

19
Q
  1. How many hydraulic servojacks does the RUDDER activate ?
    1
    2
    3
A

3

20
Q
  1. Which surfaces are used for ground spoilers ?
    All the SPOILERS
    SPOILERS 1 to 3
    SPOILERS 2 to 5
A

All the SPOILERS

21
Q
  1. With HYDRAULIC BLUE SYSTEM remaining (GREEN and YELLOW failure) and
    before LANDING GEAR EXTENSION the pitch flight control law is :
    ALTERNATE
    NORMAL
    DIRECT
A

ALTERNATE

22
Q
  1. After an AUTOMATIC RETRACTION of the flaps with CONF 1, the flaps will
    automatically reextend when speed decreases :
    Yes
    No
A

No

23
Q
  1. How many electric motors can control the stabilizer hydraulic motors ?
    1
    2
    3
A

3

24
Q
  1. Which signals cause RUDDER PEDAL movement ?
    YAW DAMPING signals
    RUDDER TRIM signals
    TURN COORDINATION signals
A

RUDDER TRIM signals

25
Q
  1. Lift augmentation is achieved on each wing by :
    3 FLAP surfaces + 4 SLAT surfaces
    2 FLAP surfaces + 5 SLAT surfaces
A

2 FLAP surfaces + 5 SLAT surfaces

26
Q
  1. SLAT retractation from 1 to 0 is inhibited if angle of attack exceeds 8°5 or
    air speed < 148 kts :
    Yes
    No
A

Yes

27
Q
  1. What happens when SFCC 1 fails ?
    Nothing
    FLAPS and SLATS operate at half speed
    FLAPS system lost
A

FLAPS and SLATS operate at half speed

28
Q
  1. In normal law, the FLIGHT MODE changes to the FLARE MODE when passing :
    50 ft
    100 ft
A

50 ft

29
Q 
187. If neither ELAC 2 nor ELAC 1 are available, pitch control is automatically transferred to
\:
SEC 2 or SEC 1
SEC 1 or SEC 3
SEC 3
A

SEC 2 or SEC 1

30
Q
  1. The pitch normal law provides :
    Manoeuvre protection + pitch attitude protection + high speed protection
    Manoeuvre protection + high angle of attack protection + high speed protection
    Load facteur limitation + high angle of attack + high speed + pitch attitude
A

Load facteur limitation + high angle of attack + high speed + pitch attitude

31
Q
  1. In alternate law, the change to direct law occurs when :
    LANDING GEAR down or at the selection of FLAPS 1 (LGCIU 1 + 2 FAULT)
    LANDING GEAR down
    Passing 50 ft
A

LANDING GEAR down

32
Q
  1. The roll normal law provides combined control of the :
    AILERONS + SPOILERS 2 to 5 + RUDDER
    AILERONS + SPOILERS 1 to 5
A

AILERONS + SPOILERS 2 to 5 + RUDDER

33
Q
  1. If ELAC 1 and 2 have failed :
    Pitch control is provided by the FAC’s
    Pitch control can only be achieved from the TRIM WHEEL
    The elevator and PITCH TRIM are controlled by SEC 2 or 1
A

The elevator and PITCH TRIM are controlled by SEC 2 or 1

34
Q
  1. When alternate law without protection is active, the high speed and high angle of
    attack protections are :
    Degraded
    Lost
A

Lost

35
Q
  1. If ELAC 1 and ELAC 2 have failed :
    ROLL CONTROL is provided by ailerons only
    ROLL CONTROL is provided by AILERONS and SPOILERS
    ROLL CONTROL is provided by SPOILERS only
A

ROLL CONTROL is provided by SPOILERS only

36
Q
  1. With GREEN and YELLOW HYDRAULIC SYSTEMS lost, manual pitch TRIM is :
    Available
    Lost
A

Lost

37
Q
  1. If YELLOW SYSTEM is lost, the FLAPS are :
    Normal
    Slow
    Lost
A

Slow

38
Q
  1. If the GREEN SYSTEM is lost, SLAT operation is :
    Normal
    Slow
    Lost
A

Slow

QT A320 (21 decks)

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