Flight Controls Flashcards

1
Q

Which yoke is connected to the right aileron

A

First officer’s

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2
Q

Which yoke is connected to the left aileron

A

Captain’s

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3
Q

How are the ailerons, elevators and rudder actuated

A

system of cables and pulleys that connect to pull and push rods at the flight control which operate a hydraulic PCU (power control unit) which hydraulically actuates the control surface

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4
Q

Which yoke controls the right elevator

A

First officer’s

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5
Q

Which yoke controls the left elevator

A

Captain’s

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6
Q

What is the purpose of the Multifunction Spoilers (MFS)

A

To assist with roll control and serve as a spoiler in flight and on landing

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7
Q

Are the Multifunction spoilers operational at any speed

A

Yes

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8
Q

How are the MFSs controlled when used for roll assistance

A

The FO’s yoke position sends an electrical signal to the left MFS panels which are hydraulically operated by PCUs. The CA’s yoke position sends an electrical signal to the right MFS panels which are hydraulically operated by PCUs

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9
Q

What is the flight deck indication of a jammed aileron cable

A

Both yokes will be jammed

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10
Q

What happens after the ROLL DISC handle is pulled

A

The aileron cable and pulley systems are disconnected through torque tubes. 20 seconds later, if the operable side has not been selected, the amber ROL SEL switchlight illuminates

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11
Q

How is the operable side selected

A

By pushing the ROL SEL/PLT ROL switchlight on the unjammed side

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12
Q

What does pushing the ROL SEL/PLT ROL switchlight accomplish

A

Allows the pilot with the operable aileron to control the on-side MFS panels

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13
Q

What is the flight deck indication of an aileron PCU runaway

A

Aircraft begins an uncommanded roll and the PLT SEL switchlight on the side without the PCU runaway illuminates automatically because of the bungee break-out signal

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14
Q

What is occurring when the pilots trim the ailerons or rudder

A

The control surface is being repositioned. There are no trim tabs

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15
Q

What panels are part of the GND LIFT dumping system

A

Inboard and outboard ground spoilers,

all 4 MFS panels

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16
Q

How are the flight controls gust locked

A

Hydraulic fluid is trapped during shutdown

17
Q

How is the Yaw Damper engaged

A

YD1 and YD2 engage switchlights on the

center pedestal

18
Q

How is the Yaw Damper disengaged

A

DISC button on the center pedestal

19
Q

What controls the yaw damper

A

The flight control computer

20
Q

Is it necessary to disconnect the Yaw Damper

on landing

A

No

21
Q

How are the flaps operated

A

Electrically

22
Q

How many flap segments does the CRJ have

A

4 total, 2 on each wing

23
Q

Is there any asymmetrical protection within the flaps

A

Yes, if the flap segments differ by > 5 degrees, the brakes are applied and the flaps will remain at the current position

24
Q

How is STAB TRIM operated

A

Electrically. A split switch on the control yoke operates two motors and a jack screw
changing the horizontal stabilizer angle of incidence

25
Q

What systems can operate the STAB TRIM

A

CA’s trim switches,

FO’s trim switches, autopilot and MACH trim

26
Q

What is the priority for STAB TRIM control

A

CA
FO
Autopilot
MACH trim