27 Flight Controls Flashcards

1
Q

Where is the flap gearbox located?

A

Forward side of the rear spar.

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2
Q

At what split will the flap safety mechanism cut power to the gearbox?

A

3 to 6 degree’s

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3
Q

How is the flap indicator operated?

A

By a potentiometer driven by the right inboard flap.

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4
Q

How many flaps and jackscrews are located on the flap system?

A

2 on flaps on each wing and 2 jackscrews on each wing.

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5
Q

What means of stops are there for the primary flight controls and trim.

A

Positive stops on the flight control surfaces and stops attached to the trim cables.

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6
Q

How many trim tabs are there for the aileron system?

A

Fixed trim tab on the RH aileron and moveable trim tab on the LH aileron assembly.

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7
Q

Where are the trim stops located for the aileron trim system?

A

On the cables themselves and stop fairleads.

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8
Q

Where are the rudder trim stops attached?

A

Fairleads

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9
Q

What size cables drives the aileron trim system?

A

1/16

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10
Q

Rudder boosts will react depending on the differential of torque from the torque transducers, what happens when it senses an engine out.

A

The flight control system provides a drive signal to the servo proportional to torque differential, higher diff = more rudder input voltage.

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11
Q

What does the elevator system have to help stability?

A

2 downforce springs attached to the bellcrank.

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12
Q

The flap lift transducer/stall warning provides the pilot of a pre stall condition, what changes the activation level of the warning tone?

A

Flap position

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13
Q

What components make up the stall warning system?

A

Lift computer, lift transducer, aural, left squat switch, stall warning self test, 5A CB, heat panel, heat control relay, 15A toggle switch.

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14
Q

What power requirements does the lift transducer need? 10 VAC

A
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15
Q

What helps prevent over travel of the flap system?

A

2 sets of motor windings

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