EMB120 Flight Controls Flashcards

1
Q

How are the elevators actuated?

A

cable and pully

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2
Q

How are the ailerons actuated?

A

cable and pully

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3
Q

How is the rudder actuated?

A

Hydraulically

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4
Q

What does the control disconnects do?

A

disconnects one side of the ailerons or elevators for the other

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5
Q

What side of the elevators system is the AP servo on?

A

Left side

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6
Q

What side of the elevator system is the pusher servo on?

A

right side

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7
Q

What side of the aileron system is the AP servo on?

A

Left side

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8
Q

How many rudder the airplane have?

A

2

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9
Q

if we loose both hydraulic systems can we still move the rudders

A

yes, In case of both hydraulic system failure, the PCU automatically reverts the rudder system to
mechanical mode

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10
Q

Will we still have rudder trim if we loose the hydraulic or the rudder PCU?

A

no the trim will fail in its last position

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11
Q

What are the rudder peddles connected to?

A

the rudder PCU

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12
Q

Can one rudder move farther than the other?

A

yes, the farther aft rudder can move farther then the other

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13
Q

does both hydraulic systems power the rudder?

A

Yes.

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14
Q

are both hydraulic systems powering the rudder during the entirety of the flight?

A

No, the green system shut shuts down at 120 knots

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15
Q

What light will turn on if the the green system doesn’t shut down at 120 knots

A

the over boost light

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16
Q

What does the rudder speed light mean?

A

there is a disagreement between the airspeed indicators at 120 knots

17
Q

what does the panel flap indication depict?

A

the average of all the flaps position

18
Q

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

A

7 degrees

19
Q

How many stall protection systems does the aircraft have?

A

2, Left and Right

20
Q

When does the pusher disconnect automatically during flight?

A

TO/Landing to prevent inadvertent push over

21
Q

How can the pilots disconnect the pusher?

A

push and hold the AP disconnect/ red waffle button