Flight Controls Flashcards

1
Q

EMB 120 has how many rudders

A

2

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2
Q

The rudder system may be actuated by

A

Green and blue hydraulic system
Green or blue hydraulic system
Mechanically by a push rod

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3
Q

The hydraulic rudder system may be turned On or OFF by the pilot

A

True

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4
Q

During normal operation above 120 knots, what hydraulic system operates the rudder

A

Blue

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5
Q

If airspeed is above 120 knots and both hydraulic systems remain connected to the ruder, what cockpit indication will the pilot see

A

OVERBOOST

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6
Q

On the ground, the rudder is held securely in place with the gust lock

A

False

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7
Q

Rudder trim is

A

A hydraulic function

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8
Q

Ailerons are actuated by means of

A

A cable and rod assembly

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9
Q

The left aileron may be operated independently by disconnecting one from the other in case of a stuck or jammed aileron

A

True

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10
Q

With the disconnected system actuated, the left aileron jammed, and the autopilot engaged, the aircraft is controllable with autopilot

A

False

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11
Q

The autopilot servo is connected to

A

The left aileron actuator

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12
Q

With the disconnect system actuated, the copilot’s control wheel operates

A

The right aileron and right elevator

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13
Q

The elevator is actuated by means of

A

A cable and rod assembly

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14
Q

If the elevator is jammed and the disconnect system actuated and only the pilot’s side was free, the stall warning system would still be completely operational

A

False
Stick shaker and autopilot is on pilot’s side
Stick pusher on copilot’s side

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15
Q

Trim is available

A

Roll, pitch and yaw

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16
Q

The airplane is equipped with, how many flap panels per wing

17
Q

Flaps are actuated by

A

A hydraulic assembly

18
Q

Flap setting positions are

A

0 and 15
15 and 25
25 and 45

19
Q

The outboard pair of flaps is actuated by what hydraulic system

20
Q

An asymmetrical flap condition occurs when

A

Two flap panel in the same pair differ in position of more than 7°

21
Q

A flap disagreement condition occurs when

A

One pair of flaps does not respond to a control signal

22
Q

What method or indication does the pilot have to determine a flap position malfunction

A

View the analog flap position
View FLAP annunciator panel

23
Q

What MAP light indicates that aileron or elevator disconnect was was actuated

A

CONTROL DISENG

24
Q

Can you reset control disconnect in flight

25
What system controls both rudders
Hydraulic
26
If we loose both hydraulic systems do we still have ruder control
Yes trough feedback manual reversion
27
If we loose both hydraulic systems do we still have rudder trim
No, trim is a hydraulic function
28
OVERBOOST light
Green system did not disconnect above 120 knots
29
RUDDER SPEED SW
Disparity between airspeed indicators. Green system may have not disconnected above 120 knots
30
At airspeeds above 120 knots you loose blue hydraulic system. Will you have rudder control
Yes green system automatically turns on
31
If you take off without testing a stall warning system, do you still have stall protection
Yes
32
Can you test stall waring system in flight
No due to landing gear proximity switch logic
33
What does analog flap position depict
Average flap position
34
How many stall protection system does the aircraft have
2
35
When does the pusher disconnect automatically turns on
5 second delay during takeoff to prevent inadvertent push over In curse below 153 knots (turns off above 173 knots)
36
At what degree in difference will a flap pair have an asymmetry
7 degrees
37
What side of the elevator system is AP on
Right side
38
What side of the elevator system is the pusher servo on
Left side
39
What side of the aileron system is AP on
Left side