Systems: Flight Controls Flashcards

1
Q

5 Spoilers on each wing

Which used for each spd brakes, roll, ground spoilers

A

Spd Brakes - 2,3,4
Roll - outer 4
Ground spoilers - All 5

Verify

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2
Q

ELAC Duties
(PAR AAA)

A
  • Pitch
  • Abnormal Attitudes
  • Roll
  • Aileron droop
  • Autopilot acquisition
  • Activates the protections
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3
Q

FAC Duties
(Be SWiFT RATTY)

A
  • Beta target
  • “Speed, speed, speed”
  • Wind shear
  • Flight Envelope Protections
  • Tail:
  • Rudder limiting
  • Alternate law yaw
  • Trim for THS
  • Turn coordination
  • Yaw damping
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4
Q

Flap Auto Retraction System (ARS)

A

In CONF 1+F the FLAPS (not slats) will automatically retract to 0 at 210 kts

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5
Q

FLAPS / SLATS

Q:​ What happens to the​ ailerons when​ the flaps are​ extended? ​

A

Ref: (FOM VOL. III-DSC-20-10-20)​ ​

The​ ailerons​ droop​ 5˚

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6
Q

FLAPS / SLATS

Q:​ When the​ FLAP legend appears​ in cyan on the​ upper ECAM​ display​ what​ is indicated?​ ​

A

Ref: (FOM VOL. III-DSC-27-30-20)​ ​

Flaps/slats in transit

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7
Q

FLAPS / SLATS

Q:​ With only​ Green hydraulic system​ pressure available,​ will​ both​ the​ flaps​ and slats operate?​ ​

A

Ref: (FOM VOL. III-DSC-27-30-10)​ ​

Yes,​ at​ ½ speed

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8
Q

How may Slat/Flap Control Computers (SFCC) are installed?

A

2

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9
Q

If one spoiler becomes faulty or inhibited, what happens to opposite spoiler?

A

The faulty one is retracted and the opposite side is retracted to prevent asymmetry.

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10
Q

Let’s assume the FO presses his take over pb and releases it after more than 40 secs…

A

The Capt’s sidestick is de-activated unless he presses his take over pb.

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11
Q

SEC Duties
(PAR SS)

A
  • Pitch
  • Abnormal attitudes
  • Roll
  • Speed brakes
  • Spoilers
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12
Q

SPEED BRAKES / SPOILERS

Q:​ At touchdown with reverse​ selected and only​ one​ landing gear strut compressed,​ will​ the​ ground ​spoilers​ extend?​ ​

A

Ref: (FOM VOL. III-DSC- 27-10-20) ​

Partially​ –​ Full​ extension​ is limited until​ both​ main​ gear​ struts​ are​ compressed

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13
Q

SPEED BRAKES / SPOILERS

Q:​ In flight, what​ happens if​ a spoiler fault​ is detected or electrical power is lost?​ ​

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​

The​ spoiler automatically​ retracts

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14
Q

SPEED BRAKES / SPOILERS

Q:​ Is​ there​ any landing​ configuration when speed​ brake​ extension is inhibited?​ ​

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​

Flaps FULL

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15
Q

SPEED BRAKES / SPOILERS

Q:​ What is​ the​ difference​ between the​ A319 - A321​ and A320​ regarding speed brake​ usage​ with the​ AP ​on?

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​ ​ ​ ​ ​ ​ ​ ​ ​ ​ ​

With the​ A319​ and 321​ you​ get full spoiler deflection​ and with the​ A320​ you only get partial​ ​spoiler deflection

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16
Q

SPEED BRAKES / SPOILERS

Q:​ When do the​ Ground​ Spoilers​ automatically extend?​ ​

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​

  • Partial​ –​ When reverse​ thrust is selected on at least one​ engine​ with​ the​ other​ at idle​ and one ​main landing​ gear strut is​ compressed​ ​
  • Full​ –​ At touchdown of both main gear​ ,​ or in​ case​ of​ RTO with airspeed above 72​ knots,​ when ​BOTH thrust levers at IDLE (if ground​ spoilers armed)​ or when reverse thrust is​ selected on​ at ​least one engine with the​ other​ thrust lever at IDLE (if​ the ground spoilers​ are​ not armed)
17
Q

SPEED BRAKES / SPOILERS

Q:​ When is speedbrake extension inhibited (SAFET)?​ ​

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​

  • SEC 1​ and​ 3​ have​ failed​ ​
  • AOA protection is active ​
  • Flaps FULL​ ​
  • Elevator (L​ or R)​ fault​ (only​ spoilers​ 3 and 4 are​ inhibited) ​
  • Thrust​ levers​ above​ the​ MCT​ position
18
Q

SPEED BRAKES / SPOILERS

Q:​ When will​ the​ ground spoilers​ automatically retract?​ ​

A

Ref: (FOM VOL.​ III-DSC-27-10-20)​ ​

When at least one​ thrust lever is​ advanced above​ IDLE

19
Q

Speedbrakes Inhibited
(SEAFAT)

A
  • SEC 1 AND 3 fault
  • Elevator L or R fault
  • Alpha Protection active
  • Flaps Full
  • Alpha Floor active
  • Thrust Levers > MCT
20
Q

The steering hand wheels can steer the nose wheel up to how much in each direction?

A

75º

21
Q

TRIMMABLE HORIZONTAL STABILIZER

Q: How is the​ THS normally operated​ in flight? ​ ​ ​ ​ ​ ​ ​ ​ ​ ​

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​

The​ flight control computers​ control trim​ functions automatically

22
Q

TRIMMABLE HORIZONTAL STABILIZER

Q:​ Can you​ move​ the​ PITCH​ trim wheel if​ all​ systems​ are​ working normally?​ ​

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​

Manual​ inputs​ have​ priority​ over​ computer inputs.​ The​ autopilot will​ disconnect

23
Q

TRIMMABLE HORIZONTAL STABILIZER

Q:​ If​ a complete​ flight control computer failure​ occurs​ can the​ THS​ be​ positioned? ​

A

Ref: (FOM VOL. III-DSC-27-10-20)​ ​

Yes,​ mechanical trimming is​ possible​ by​ manually​ positioning the​ Pitch Trim​ Wheel

24
Q

TRIMMABLE HORIZONTAL STABILIZER

Q:​ If​ NO hydraulic power is available can the​ THS be positioned?​ ​

A

Ref: (FOM VOL. III-DSC-27-10-10)​ ​

No - the​ THS​ requires​ hydraulic power from the​ Green or​ Yellow systems

25
Q

TRIMMABLE HORIZONTAL STABILIZER

Q:​ What happens to the​ THS when the​ aircraft enters into Ground​ Mode?​ ​

A

Ref: (FOM VOL. III-DSC-27-20-10-20)​ ​ ​

The​ trim automatically​ resets to zero​ (inside​ the​ green​ band)

26
Q

What are the two configurations produced by position 1 on the flaps lever?

A
  • 1+F (Slats and Flaps) for takeoff
  • 1 (Slats Only) in flight
27
Q

What does a
WING TIP BRK ON
message on the E/WD indicate?

A

A hydraulic device locks the flaps in their present position.

28
Q

What system prevents flap or slat asymmetry?

A

Wing Tip Brakes (WTB)

29
Q

What would happen if one of the two SFCC’s failed?

A

Slats and flaps operate at half speed

30
Q

When using the​ rudder pedals​ for steering, when does​ the steering angle​ begin to reduce?​

A

Starts reduction​ at 40 knots​ and progressively​ reduces​ to zero degrees at​ 130​ knots

31
Q

WINGTIP BRAKES
(ROAM)

A
  • Runaway of surface
  • Over speed of mechanism
  • Asymmetry
  • Movement of surface un-commanded