Flight Controls

Question 1

Hydraulic System _____ normally power(s) the primary flight controls.

Answer 1

A and B

Question 2

Loss of Hydraulic Systems A and B render _____ spoiler

panels inoperative.

Answer 2

Correct Answer 1

1) all

Question 3

Ailerons and elevators operate _____ with loss of both

Hydraulic Systems A and B.

Answer 3

manually

Question 4

Roll control surfaces consist of _____ powered _____.

Answer 4

hydraulically / ailerons and flight spoilers

Question 5

Positioning FLT CONTROL A switch to STBY RUD ______.

Answer 5

activates Standby Hydraulic Pump and opens Standby

Rudder Shutoff Valve

Question 6

The rudder operates with _____ during Manual Reversion.

Answer 6

the Standby Hydraulic System

Question 7

Pushing a single Left Wing Down or Right Wing Down

AILERON trim switch ______.

Answer 7

does nothing

Question 8

Aileron trim applied with the autopilot engaged ______.

Answer 8

may cause abrupt rolling movement when disconnecting

the autopilot

Question 9

More than _____ (approximately) control wheel

displacement (in degrees) initiates spoiler deflection.

Answer 9

10°

Question 10

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

Answer 10

SPOILER A and B

Question 11

With a jammed Spoiler System”,” the _____.

Answer 11

Captain provides roll control with the ailerons

Question 12

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

Answer 12

First Officer provides roll control using the Flight Spoilers.

Question 13

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

indicates ______.

Answer 13

excessive differential pressure in the Elevator Feel

Computer

Question 14

Actuating either pair of Stabilizer Trim Switches on the

control wheels”,” with the autopilot engaged ______.

Answer 14

disconnects the autopilot

Question 15

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

Answer 15

OVERRIDE / control column

Question 16

The green band of the STAB TRIM indicator on the Control Stand indicates the ______.

Answer 16

takeoff trim limits

Question 17

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

Master Caution Recall”,” indicates _____ failure.

Answer 17

a single FCC channel

Question 18

Two independent Stall Management Yaw Damper (SMYD)

computers provide _____.

Answer 18

outputs for all stall warnings in flight

Question 19

Selecting FLT CONTROL A or B switch to STBY RUD activates the Standby Hydraulic Pump and arms the _____ light(s).

Answer 19

LOW PRESSURE

Question 20

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

Answer 20

at speeds above approximately 135kts

Question 21

The RUDDER trim control electrically repositions the Rudder Feel and Centering Unit and _____ the rudder pedals.

Answer 21

displaces

Question 22

The Standby Yaw Damper operates with ______.

Answer 22

both FLT CONTROL switches positioned to STBY RUD and the YAW DAMPER switch reset to ON

Question 23

Positioning the Speed Brake Lever to UP”,” _____”,” extends the _____ Spoilers to their maximum position.

Answer 23

on the ground only / Ground and Flight

Question 24

The SPEED BRAKE DO NOT ARM light (amber) indicates

_______.

Answer 24

an abnormal condition or abnormal test inputs to the

Automatic Speed Brake System

Question 25

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

Answer 25

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

Question 26

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

for ______.

Answer 26

Correct Answer 4
1) 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

Question 27

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

Answer 27

fully extend

Question 28

The LE slats _____ when moving the FLAP lever beyond

_____ degrees.

Answer 28

deploy to full extend / 25

Question 29

The flap load relief system is operational at ______.

Answer 29

Flaps 10, 15, 25, 30 & 40

Question 30

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

Answer 30

LE Slats / stick shaker

Question 31

AUTO SLAT FAIL light (amber) Illumination during Master

Caution Recall indicates a failure of _________.

Answer 31

a single Stall Management Yaw Damper (SMYD)

Question 32

Momentarily positioning Alternate Flaps switch DOWN fully extends the ______ using the _____ Hydraulic System.

Answer 32

LEDs / Standby

Question 33

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

Answer 33

fully extend

Question 34

Selecting UP on the ALTERNATE FLAPS position switch_____.

Answer 34

electrically retracts the TE flaps