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EMB 120 > Flight Controls > Flashcards

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

A

Three

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

A

Green

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

A

No

25
Q

What system controls both rudders

A

Hydraulic

26
Q

If we loose both hydraulic systems do we still have ruder control

A

Yes trough feedback manual reversion

27
Q

If we loose both hydraulic systems do we still have rudder trim

A

No, trim is a hydraulic function

28
Q

OVERBOOST light

A

Green system did not disconnect above 120 knots

29
Q

RUDDER SPEED SW

A

Disparity between airspeed indicators. Green system may have not disconnected above 120 knots

30
Q

At airspeeds above 120 knots you loose blue hydraulic system. Will you have rudder control

A

Yes green system automatically turns on

31
Q

If you take off without testing a stall warning system, do you still have stall protection

A

Yes

32
Q

Can you test stall waring system in flight

A

No due to landing gear proximity switch logic

33
Q

What does analog flap position depict

A

Average flap position

34
Q

How many stall protection system does the aircraft have

A

2

35
Q

When does the pusher disconnect automatically turns on

A

5 second delay during takeoff to prevent inadvertent push over
In curse below 153 knots (turns off above 173 knots)

36
Q

At what degree in difference will a flap pair have an asymmetry

A

7 degrees

37
Q

What side of the elevator system is AP on

A

Right side

38
Q

What side of the elevator system is the pusher servo on

A

Left side

39
Q

What side of the aileron system is AP on

A

Left side

EMB 120 (22 decks)

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