Flight controls Flashcards

1
Q

What flight controls do we have on each wing?

A

5 x slats
5 x spoilers
2 x flaps
1 x aileron (at the end of the wing)

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2
Q

How are the flight controls - controlled and then actuated?

A

Fly by wire

“All flight controls are ELECTRONICALLY CONTROLLED and HYDRAULICALLY activated”

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3
Q

How does the flight control system work

A

(Caution - check answer)

  1. Demand made by pilot
  2. Goes to F/CTR computer
  3. Signal sent to actuator
  4. Actuator moves surface
  5. Response feedback back to F/CTR computer

Note: in normal law the computers prevent excessive manoeuvres and keeps us inside the flight envelope in the pitch and roll axis

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4
Q

Flight control - side stick

Are the FO AND CAPT side sticks mechanically linked?

A

No - they are not mechanically linked

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5
Q

Side stick - what is the SOP for disconnecting autopilot in flight?

A

Side stick red push button.

Why? Because this prevents an ECAM warning (albeit you still get the cavalry noise)

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6
Q

Side stick - Dual Inputs

A

They are algebraically added. Therefore:

  1. Half side deflection from CAPT plus half side stick deflection from FO (in same direction) = full deflection
  2. Full bank left from CAPT and full bank right from FO = no deflection

When doing flight control check (during taxi) - remember to look at the ECAM display (not the PFD)

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7
Q

Side stick - Priority

What is shown if Capt takes priority from the PF?

A
  1. Red arrow appears in front of the person that lost control (FO) and points to the person that has control (Capt)
  2. A green “CAPT” light illuminates (I.e says who now has control)
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8
Q

Side Stick - how do you take control from copilot?

A

Press and hold red pb for 40 seconds (this then semi locks out the co-pilot)

Does not fully lock because the co-pilot could request control back again

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9
Q

Rudder Trim Switch. What is the impact of autopilot on?

A

Autopilot on - turning the trim knob on the pedestal has no impact

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10
Q

What are the Cockpit THS controls? What happens if you manually control them in cockpit

A

2 x THS Hand wheels

If grab, you override the automatic computer and are directly controlling the electric motors which in turn move THS

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11
Q

What flight control computers does the a320 have?

A

Caution - not sure if below is 100% correct yet

  1. 2 x ELAC [Elevator and Aileron Computer]
  2. 3 x SEC [Spoiler and Elevator Computer] (note: also controls the standby elevators and stab control)
  3. 2 x FAC [Flight Augmentation Computer]

Not a computer as such but there are also:

2 x FCDC [Flight Computer Data Concentrators]

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12
Q

Elevators. Basic components of the system?

A

Each elevator is:

  1. Driven by 2 x electrically controlled hydraulic servo jacks
  2. Only 1 servo jack active at a time (the other is in damping mode)
  3. Left Elevator (Green Hyd). Right Elevator (Yellow Hyd) [Instructor advised don’t need memorise colours]
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13
Q

Elevators - how do they work in normal conditions?

A

There are 2 servojacks per elevator

A) 1 x servojack does all of the work; and

B) 1 x servo-Jack “relaxes” and simply follows what the other is doing (“Damping mode”) [instructor likened it to floating around)

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14
Q

Elevators - how do they work in abnormal (neither hydraulic Jack being controlled electrically)?

A

Reverts to “Central Mode” (elevator locks at the central / neutral position)

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15
Q

Elevators. What modes do the servojacks have?

A
  1. Active (the servojack is electronically controlled)
  2. Damping (the jack follows the surface movement)
  3. Centering (elevator locks at center/neutral)
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16
Q

Elevators - Pitch control.

Re computers. How is the system controlled in normal and abnormal?

A

Normal = controlled by ELAC 2 (for both left and right elevators)

Abnormal (I.e. ELAC 2 fail) = ELAC 1 active

Abnormal (lose both ELAC 1 and 2) - control reverts to SEC 1 and then SEC 2

17
Q

Stabilisers (pitch control)

How are they controlled?

A
  1. Operated by a screw jack
  2. Screw Jack driven by 2 x Hydraulic motors (Green and Yellow)
  3. Hydraulic motors controlled bya) one of three electric servo motors (depending on which is controlling); OR
    b) the mechanical trim wheel (which will override point a)
18
Q

Which parts of wing are used for roll control (per wing)?

A

Each wing has/uses:

  1. 4 spoilers (2-5) [i.e all of the outboard ones]
  2. 1 aileron
19
Q

What are the three different spoiler configurations for a) roll b) speed brakes (in the air) c) speed brakes (ground)?

A

A) roll = 1 x aileron and 4 x spoilers (nos 2-5)

B) speed brakes (air) = 3 x spoilers (no. 2-4) [middle ones]

C) Speed brakes (ground) = all 5 spoilers

Key point: only the no. 1 spoiler (inboard) is ever used on the ground

20
Q

Which computer controls ailerons?

A

ELACs

21
Q

Ailerons. What is the backup if both ELACS inop?

A

None. There is no back up

22
Q

What computer controls the spoilers?

A

SEC (Spoiler Elevator Computer)

(Note: Each spoiler (per wing) is controlled by an individual SEC)

23
Q

Spoilers. What happens if a left wing individual spoiler is loses Hyd pressure and inop (e.g the no.2)?

A

It will “float” (damping mode). The no.2 spoiler on the right wing will also go to damping mode (to avoid asymmetric flight)

24
Q

What is “Aileron droop”?

A

When the flaps are extended, the ailerons are extended down by 5 degrees in order to provide additional lift

25
Q

Yaw control system / computers

A
  1. Controlled by the ELACs
  2. ELACS send signals to the 3 x hydraulic jacks on the rudder
  3. The hydraulic jacks then move the rudder
26
Q

Yaw control. What controls the rudder trim?

A

2 x FACs (Flight Augmentation Computers)

27
Q

What is the Rudder Travel Limiter?

A

When you go faster there is a decrease in the rudder authority (ie the maximum rudder movement you can command from rudder pedals decreases as you faster - even with your foot to the floor!)

28
Q

What happens if the rudder travel limiter fails?

A

Caution - check below is correct

It freezes at last known position. Unlocks again during approach (when not clean config)