Flight Controls

Question 1

Do not deploy speed brakes below

Answer 1

1000 feet AGL

Question 2

Can either hydraulic system provide full power to the ailerons

Answer 2

yes

Question 3

with total hydraulic failure how are the ailerons operated?

Answer 3

reverts to mechanical control

Question 4

with jammed spoilers what can supply roll control through the ailerons?

Answer 4

force supplied to the CA control wheel provides roll control through the ailerons

Question 5

with jammed ailerons what can supply roll control through the spoilers?

Answer 5

force supplied to the FO control wheel provides roll control through the spoilers

Question 6

Is it permissible to add aileron trim with the AP engaged?

Answer 6

Prohibited, may cause abrupt rolling moment

Question 7

Spoilers deploy when how much bank is entered?

Answer 7

10° they deploy with the ailerons and remain flat on the down side

Question 8

To reposition the aileron trim to neutral

Answer 8

movement of both switches

Question 9

The elevator is ____ powered

The stabilizer is _____ powered

Answer 9

hydraulically

electrically

Question 10

How is a control jam over ridden?

Answer 10

Over ride mechanism allows the control column to be physically separated

Question 11

The FEEL DIFF PRESS light indicates

Answer 11

excessive differential hydraulic pressure is sensed in the elevator feel computer

Question 12

how does the Mach Trim system engage and disengage?

Answer 12

Automatically as a function of airspeed

Question 13

When MACH TRIM FAIL is illuminated only when the master caution annunciator recall is activated it means

Answer 13

a single channel has failed in the mach trim system

Question 14

The Elevator Feel Shift Module increase hydraulic system A pressure to the elevator feel and centering unit during a stall for what purpose?

Answer 14

To increase the forward control column force to approximately double the normal feel pressure to try to assist in not stalling the plane

Question 15

There are two mode on the main electric and autopilot stabilizer trim,

Answer 15

high speed flaps extended

low speed flap retracted

Question 16

if the autopilot is engaged actuating either pair of stabilizer trim switches

Answer 16

disengages the autopilot

Question 17

if takeoff is attempted with the stabilizer trim outside the take off limits what can one expect

Answer 17

a intermittent horn, (takeoff config horn)

Question 18

If manual trim is used to trim beyond the electrical trim limits can the stab trim be used to return it to normal limits

Answer 18

yes

Question 19

The stab trim main electric cutout switch and the stab trim autopilot cutout switch are provided to allow the autopilot or main electrical trim input to be

Answer 19

disconnected from the single stab trim motor

Question 20

when the control column movement opposes the trim direction what will occur?

Answer 20

The control column actuated stabilizer trim cutout switches stop operation to the main electric and autopilot trim.

Question 21

Switching the Stab trim into OVERRIDE

Answer 21

the electric trim can be used regardless of control column position

Question 22

the speed trim system is a speed stability augmentation system designed to improve the flight characteristics during any operation

Answer 22

Low gross weight, aft CG, and high thrust when the autopilot is not engaged

Question 23

Both hydraulic systems operate the rudder

Answer 23

including the standby

Question 24

What hydraulic system is the yaw dampener associated with?

Answer 24

system B and the standby system

Question 25

135 knots and above the hydraulic pressure is reduced to limit the rudder authority

Answer 25

it provides the controls necessary for the stages of flight.

Question 26

Using the rudder pedals for steering how much displacement is capable?

Answer 26

7° either side of center

Question 27

when the speed brake lever is actuated on the ground or in the air

Answer 27

ground all spoilers deploy | air on the in flight spoilers

Question 28

which hydraulic system powers the ground spoilers

Answer 28

A

Question 29

if spoilers are deployed in a turn

Answer 29

the rate of roll increases greatly

Question 30

All spoilers will automatically deploy to full on landing if

Answer 30

the speed brake lever is armed and | the thrust lever are in idle

Question 31

SPEEDBRAKE DO NOT ARM light indicates

Answer 31

abnormal condition or wheel speed is below 60 knots and the speed brake lever is not in the down position.

Question 32

Whats the difference between Flight Detent and Up on the spoiler lever

Answer 32

Flight Detent full spoiler deployment in the air | Up all flight and ground full spoilers deployment on the ground

Question 33

Can the Trailing edge flaps be operated with full hydraulic failure?

Answer 33

Yes, electrically

Question 34

is there asymmetrical or skew protection of the trailing edge flaps electrically?

Answer 34

No

Question 35

The Flaps Slats Electrical Unit (FSEU) monitor trailing flap to

Answer 35

Monitor asymmetry or skewing. It closes the trailing edge bypass valve if it senses it.

Question 36

The Trailing Edge (TE) flap load relief protects the flaps from excessive loads

Answer 36

When the flaps are at 40 and excessive AS exceeds a predetermined limit it retracts the flaps to 30

Question 37

What are the flap gates for at 1 and 15?

Answer 37

Single Engine and Normal Go around

Question 38

Where would one find the TE flap asymmetry indications?

Answer 38

Back overhead panel, Flap Position Indicator

Question 39

LE devices are normally extended and retracted by

Answer 39

Hydraulic system B

Question 40

Can the LE devices be retracted in Standby

Answer 40

No

Question 41

flaps 1 the Auto Slat system automatically drive the slats to FULL EXTENDED as the plane approaches

Answer 41

a stall condition

Question 42

Amber light LE FLAP TRANSIT indicates

Answer 42

LE slat skew condition exist | LE device in transit or out of position with its trailing edge devices