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BAK > Flight Controls > Flashcards

Flight Controls Flashcards

1
Q

The FEEL DIFF PRESS light (amber)”,” when illuminated”,”

indicates ______.

A

excessive differential pressure in the Elevator Feel

Computer

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2
Q

The Aileron System is jammed. How is roll control provided?

A

First Officer provides roll control using the Flight Spoilers

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3
Q

Two independent Stall Management Yaw Damper (SMYD)

computers provide _____.

A

) outputs for all stall warnings in flight

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4
Q

Selecting UP on the ALTERNATE FLAPS position switch_____

A

electrically retracts the TE flaps

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5
Q

The rudder operates with _____ during Manual Reversion

A

the Standby Hydraulic System

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6
Q

Approaching the stall angle of attack”,” with Flaps 1 through
25 selected”,” the _____ automatically begin driving to full
extend prior to _____ activation

A

LE Slats / stick shaker

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7
Q

With a jammed Spoiler System”,” the _____.

A

Captain provides roll control with the ailerons

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8
Q

The flap load relief system is operational at ______.

A

Flaps 10, 15, 25, 30 & 40

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9
Q

It is possible to _____ the LEDs using the Standby Hydraulic
System with the loss of Hydraulic System B

A

fully extend

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10
Q

The Standby Yaw Damper operates with ______

A

both FLT CONTROL switches positioned to STBY RUD and

the YAW DAMPER switch reset to ON

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11
Q

More than _____ (approximately) control wheel

displacement (in degrees) initiates spoiler deflection

A

10°

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12
Q

Positioning the Speed Brake Lever to UP”,” _____”,” extends

the _____ Spoilers to their maximum position.

A

on the ground only / Ground and Flight

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13
Q

Roll control surfaces consist of _____ powered _____

A

hydraulically / ailerons and flight spoilers

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14
Q

The green band of the STAB TRIM indicator on the Control

Stand indicates the ______.

A

takeoff trim limits

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15
Q

The LE slats _____ when moving the FLAP lever beyond

_____ degrees

A

deploy to full extend / 25

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16
Q

The RUDDER trim control electrically repositions the Rudder

Feel and Centering Unit and _____ the rudder pedals

A

displaces

17
Q

SPEED TRIM FAIL light (amber)”,” illuminating only during

Master Caution Recall”,” indicates _____ failure.

A

a single FCC channel

18
Q

Selecting FLT CONTROL A or B switch to STBY RUD activates

the Standby Hydraulic Pump and arms the _____ light(s)

A

LOW PRESSURE

19
Q

Pushing a single Left Wing Down or Right Wing Down

AILERON trim switch ______

A

) does nothing

20
Q

Ailerons and elevators operate _____ with loss of both

Hydraulic Systems A and B.

A

manually

21
Q

Loss of Hydraulic Systems A and B render _____ spoiler

panels inoperative.

A

all

2) only the flight
3) only the ground
4) only the outboard

22
Q

Select the switch(es) used for maintenance purposes only.

A

SPOILER A and B

23
Q

Momentarily positioning Alternate Flaps switch DOWN fully

extends the ______ using the _____ Hydraulic System

A

LEDs / Standby

24
Q

Aileron trim applied with the autopilot engaged ______

A

may cause abrupt rolling movement when disconnecting

the autopilot

25
Q

Actuating either pair of Stabilizer Trim Switches on the

control wheels”,” with the autopilot engaged ______.

A

disconnects the autopilot

26
Q

The LE flaps _____ when moving the FLAP lever from UP to 1.

A

fully extend

27
Q

STAB TRIM switch on the Aft Electronic Panel”,” positioned
to _____”,” allows operation of the main electric trim
regardless of _______ position.

A

OVERRIDE / control column

28
Q

Hydraulic System _____ normally power(s) the primary flight

controls

A

A and B

29
Q

The Main Rudder Power Control Unit (PCU) limits full rudder

authority ______.

A

in flight

30
Q

The SPEED BRAKE DO NOT ARM light (amber) indicates

_______

A

an abnormal condition or abnormal test inputs to the

Automatic Speed Brake System

31
Q

In flight”,” the LE FLAPS TRANSIT light (amber) illuminates

for ______

A

any LE device in transit
2) any LE device not in programmed position with respect
to TE flaps
3) two (2) or more LE flaps or slats moved from their
commanded position
4) all of the above

32
Q

If the Air/Ground System does not sense main landing gear
wheels spin-up after landing”,” with the speed brake
armed”,” the flight spoilers _____.

A 
automatically deploy when Air/Ground System senses 
ground mode (any strut compresses)
33
Q

AUTO SLAT FAIL light (amber) Illumination during Master

Caution Recall indicates a failure of _________

A

a single Stall Management Yaw Damper (SMYD)

34
Q

Positioning FLT CONTROL A switch to STBY RUD ______.

A

activates Standby Hydraulic Pump and opens Standby

Rudder Shutoff Valve

BAK (17 decks)

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