A320 > Flight Controls > Flashcards

Flight Controls Flashcards

(57 cards)

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1
Q

How many FlightControl computers does the A320 have? What are they?

A
  • 7
  • ELAC 1/2 (Elevator Aileron Comp)
  • SEC 1/2/3 (Spoiler Elevator Comp)
  • FAC 1/2 (Flight Augmentation Comp)
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2
Q

Which three flight control computers remain active during an EMER ELEC CONFIG?

A
  • ELAC 1
  • SEC 1
  • FAC 1
    (All on left side of upper panel)
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3
Q

If one flight control, computer fails what happens?

A

The back up computer (ELAC/SEC/FAC) takes over automatically.

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4
Q

What happens if both ELACs fail?

A
  • Flight control laws degrade from normal to alternate law
  • Both ailerons are in operative and roll control is provided by the spoilers
  • elevator and THS control is provided by the SEC’s
  • Both auto pilots will be inoperative
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5
Q

Which spoilers are controlled by SEC 1/2/3?

A
  • SEC1: Spoilers 3/4
  • SEC2: Spoiler 5
  • SEC3: Spoilers 1/2
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6
Q

Which SEC’s provide backup elevator and THS control in case both ELAC’s fail?

A

SEC 1 and 2

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7
Q

What happens if all three SEC’s have failed or are selected off?

A
  • The speed, brakes and spoiler panels are all inoperative and roll is controlled by ailerons only
  • The ability of the FCC’s to provide back up control is lost
  • Flight control laws degrade from normal to alternate law
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8
Q

If all three, SEC’s fail or are turned off what happens to the auto pilot?

A

Nothing as information to the auto pilot is still provided by the ELAC’s and FACs.

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9
Q

What happens if both FAC’s have failed or are selected off?

A
  • Rudder control is through the rudder pedals via mechanical connection
  • Rudder trim, yaw damping, and rudder limiting are lost
  • Flight control laws degrade from normal to alternate law
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10
Q

How long does the priority take over pb need to be pressed to maintain priority without pushing the button?

A

40 sec

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11
Q

Which spoilers also provide roll control?

A

Spoilers 2-5

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12
Q

If one spoiler servo fails what happens?

A

The other side spoiler servo is deactivated to maintain symmetry

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13
Q

If the auto pilot is activated, can the rudder trim selector be used?

A

No, it is deactivated

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14
Q

If both FAC’s fail what happens to rudder travel limit?

A
  • It is initially frozen in the current position
  • rudder travel limit removed when slats are extended for approach
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15
Q

Which spoilers operate as speed breaks?

A

Spoilers 2/3/4

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16
Q

Which spoilers are used for ground spoiler operation?

A

All 5 spoilers

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17
Q

What is the maximum deflection of the speed brakes when auto pilot is engaged?

A

1/2 deflection even if speed brake lever is set to full

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18
Q

If the speed brake lever is in the full position in the auto pilot disengages, what happens?

A

The spoilers rapidly move to full deflection

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19
Q

If the spoilers in the full position in the auto pilot is engaged what happens?

A

The spoilers rapidly moved to the half deflection position

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20
Q

Can the speed brakes be used with flaps full selected?

A

No, speed brake is inhibited with flaps full selected

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21
Q

How are the slats and flaps controlled?

A

Slats and flaps control computer (SFCC)

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22
Q

What is the height limitation to extend slats/flaps?

A

FL200 (do not extend above)

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23
Q

F one SFCC fails what happens?

Study These Flashcards
A

The other SFCC takes over its function, but the slats and flaps operate at half speed

24
Q

At what speed does automatic flap retraction occur?

25
Do the slats retract when an over speed condition occurs?
No
26
What are the flight control laws?
- Normal Law - Alternate Law - Direct Law - Back up control law - Abnormal Attitude Law
27
What control are available in mechanical back up law?
- Manual pitch trim - Rudder pedals - Engine thrust
28
Beyond what bank angle does automatic pitch trim stop?
33°
29
What are the normal law protections?
- Maneuver protection - Pitch attitude protection - High speed protection - Alpha protection (angle of attack protection)
30
What is maneuver protection? What are its limits?
- It prevents the aircraft from overstressing - +2.5 G and -1.0 G (clean configuration) - +1.0 G and -0.0 G (other configuration)
31
What is pitch attitude protection and what are its limits?
- limits excessive aircraft nose up and nose down pitch - +30° nose up and -15° nose down
32
How are the pitch limits indicated on the PFD?
- green equal signs at +30° nose up in -15° nose down
33
What happens to the flight directors if the nose pitch limits a reached?
It disappears
34
What is high-speed protection and what are its limits?
- it limits aircraft speed - green equal sign just above Vmo/Mmo
35
What happens when the high speed protection limit is reached?
- The ELACs pitch up the aircraft to prevent further acceleration. - nose down automatic trim is inhibited - auto pilot disengages
36
After high-speed protection has been activated, and the sidestick is returned to neutral to what speed does the aircraft return?
Vmo/Mmo
37
What is alpha protection?
Aircraft flight control surfaces prevent the angle of attack from exceeding its limits.
38
What happens if Alpha PROT is reached?
- Pitch control changes from load demand to alpha demand - Auto pilot is disengaged - Nose up trim is inhibited
39
What speed is reached is the side stick is held to full back?
Alpha MAX
40
What is alpha floor protection?
- auto thrust system - Only available in normal law - commands TOG a thrust when triggered -
41
Up to what bank angle will the aircraft maintain the angle even if side stick pressure is released?
33°
42
To bank the aircraft beyond 33° what must the pilot do?
- Roll the aircraft to the desired bank angle and hold it there - Apply back pressure to maintain altitude
43
If you are at angles greater than 33° and release the side stick side pressure what happens?
Positive spiral stability returns the aircraft to 33° bank angle.
44
Between what bank angles does the aircraft maintain positive spiral stability?
- Greater than 33°, but less than 67° - at all Bank angles if high speed or alpha protection is active
45
If alpha or high speed protection is active to what bank angle does the aircraft return if the stick pressure is released?
0° bank angle
46
What is the bank angle protection limit?
67°
47
What is the bank angle limit if high speed or aloha protection is active?
45° bank angle
48
What happens at 45° bank angle is exceeded?
- auto pilot disconnect - Flight Director disappears
49
An approach at which altitude RA is the pitch trim frozen? At which altitude do the ELACs add a gentle nose down command?
- 50 feet AGL - 30 feet AGL
50
What Foltz in flight control computers will cause the aircraft to switch to alternate law?
- Dual ELAC faults - Dual FAC faults - Triple SEC faults - Dual hydraulic faults (except HYD B+Y SYS LO PR) - Dual ADR faults - Dual IR faults
51
How can you tell if you’re in ALT LAW?
- ECAM F/CTL ALTN LAW (PROT LOST) - Amber Xs at pitch and roll limits - Airspeed indicator changes to Red/Black indicator (no Amber alpha Prot and alpha Max indication) (top of red indicates Vsw)
52
Is high-speed protection available in ALT LAW?
No, high speed stability is still available. - A protection prevents you from exceeding a limit. - Stability only discourages you from exceeding a limit. You can always manually override a stability with sidestick input.
53
Can the aircraft be stalled?
Yes, if in ALT LAW and the side stick is held back.
54
Does alternate law provide a landing mode? What happens as a result?
No When landing gear is extended, alternate law changes to direct law
55
How can the pilot tell if the aircraft is in direct law?
- ECAM F/CTL DIRECT LAW (PROT LOST) - PFD Indicates USE MAN PITCH TRIM - Amber Xs
56
After having recovered from abnormal attitude law, what law does the aircraft return to?
ALT LAW
57
How can the pilot tell if they are in backup control law?
- PFD indicates red MAN PITCH TRIM ONLY - Red SPD SEL above speed tape - Red SPD LIM next to speed tape - Amber Xs
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