FLIGHT CONTROLS Flashcards

1
Q

Which flight controls are conventionally powered? Are the ailerons connected directly to the Captains or Co-pilots control wheel?

A

The ailerons and elevator are cable powered, the ailerons are connected to the FO control column.

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2
Q

Which flight controls are hydraulically powered?

A

Rudder, spoilers and flaps.

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3
Q

How is roll control achieved?

A

Spoilers and ailerons, the outboard spoilers lockout above 140/150kts

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4
Q

How is aileron trim applied?

A

The RH spring tab is repositioned.

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5
Q

How can you depressurise the roll spoilers?

A

Pressing the SPLR 1/2 pushlight or the INBD/OUTBD pushlights.

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6
Q

With the roll disconnect pulled, what does each control wheel control? Will SPLR 1 and SPLR 2 switch-lights illuminate in this situation?

A

The captain controls spoilers and the FO controls ailerons. The pushlights will not illuminate, they illuminate if a jam occurs.

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7
Q

What is different about the spoilers above 140kts?

A

The outboard spoilers are locked out.

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8
Q

When do the ROLL SPLR INBD or ROLL SPLR OUTBD caution lights illuminate individually?

A

If one set of spoilers gets stuck/jammed.

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9
Q

What is the source of hydraulic pressure for the rudder?

A

Both main hydraulic systems

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10
Q

What effect does airspeed have on rudder hydraulic pressure (200/300)?

A

Hydraulic pressure is limited to 900PSI above 150kts(300), 140kts(200) and is 1500PSI below

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11
Q

What happens if a rudder control system jams? Is there an airspeed reduction?

A

RUD 1/2 pushlight would be pressed and speed limited to maximum 200kts.

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12
Q

When is rudder deflection restricted?

A

The rudder is limited to 12deg deflection both ways at flap 0, full rudder operation at flap 15 or greater. (18R, 16L)

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13
Q

Is there a gust lock for the rudder? What flight controls are locked when the CONT LOCK handle is pulled to the lock position?

A

Ailerons and elevator are locked by the cont lock, it also limits NH to 84%. The rudder doesn’t have a lock.

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14
Q

How is rudder trim applied?

A

The rotary switch on the centre console. there is a fast and slow function depending on deflection of the switch. rudder can be trimmed up to 10deg from set position.

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15
Q

How is elevator trim normally applied?

A

Trim wheels either side of throttle quadrant.

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16
Q

When is the standby elevator trim system used? How is it applied?

A

The standby trim is applied by switching the guarded switch. the toggles on the pilot’s side console use the autopilot trim servo to trim the tailplane.

17
Q

What can you do if a jam occurs in the elevator system?

A

The pitch disconnect can be pulled which will allow each pilot’s control column to control their respective side elevator.

18
Q

What hydraulic system powers the flaps? With the flaps retracted how many degrees left / right is rudder travel restricted to?

A

No. 1 hydraulic system. 12Deg either side.

19
Q

How is the solenoid shutoff valve opened? How long is hydraulic pressure available to the flaps?

A

The flap selector lever sends a signal to the solenoid and this remains open for 70 seconds.

20
Q

What brings on the FLAP POWER caution light?

A

If the hydraulic pressure is less than 1500PSI, or the valve is open greater than 70seconds.

21
Q

What will bring on the FLAP DRIVE caution light?

A

If the primary flap drive fails.

22
Q

How many stall warning systems are there? Does flap position have any effect on stall warning?

A

2 stall warning systems which compensate for flap.

23
Q

What indication is there of stall warning computer failure?

A

L/R stall warn caution light will illuminate aswell as the master caution.

24
Q

If a stall warning computer fails, will the system still operate 200/300?

A

Yes(300)

25
Q

What will be the flight deck indication of a jammed aileron cable?

A

The control wheel will not rotate.

26
Q

What does a ROLL SPOILER INBD/OUBD HYD caution mean?

A

Loss of pressure to the respective spoiler.