Flight Controls Flashcards

1
Q

What are the three axes of flight?

A
  • Longitudinal (roll)
  • Vertical (yaw)
  • Latitudinal (pitch)
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2
Q

What are the two kinds of flight controls?

A
  • Primary

- Secondary

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3
Q

How are all of the flight controls operated?

A

Manually

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4
Q

What are the primary flight controls?

A
  • Ailerons
  • Elevator
  • Rudder
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5
Q

What are the secondary flight controls?

A
  • Aileron trim surfaces (roll)
  • Elevator trim tab (pitch)
  • Rudder trim tab (yaw)
  • Trim Aid Device (TAD)
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6
Q

How are the secondary flight controls operated and controlled?

A

Electromechanically

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7
Q

What are the components of the aileron control system?

A
  • Left and right aileron
  • Two control sticks
  • Interconnect tubes
  • Push-pull rods
  • Bellcranks
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8
Q

Who adjusts the aileron trim tab?

A

Maintenance personnel only

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9
Q

What are the components of the elevator system?

A
  • Elevator
  • Two control sticks
  • Push-pull rods
  • Interconnect tube
  • Bellcranks
  • Elevator cables
  • Downsprings
  • Bobweight
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10
Q

What is the bobweight used for?

A

Provides extra weight to give a heavier stick force whenever G-loading is increased. This helps enhance control feedback to help prevent overstressing

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11
Q

What are the components of the rudder system?

A
  • Rudder
  • Two control sticks
  • Two sets of rudder pedals
  • Rudder cables
  • Pulleys
  • Bellcranks
  • Tie rods
  • Centering springs
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12
Q

What does a properly trimmed aircraft do?

A

Greatly reduce pilot workload and fatigue

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13
Q

Who has priority in the event of conflicting trim inputs?

A

Rear cockpit

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14
Q

What happens when the trim interrupt button is pressed and held?

A
  • Trim disconnects
  • TRIM OFF annunciator illuminates
  • TAD OFF annunciator illuminates
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15
Q

What happens when the trim interrupt button is released?

A
  • Power is restored to the trim actuators
  • TAD OFF annunciator remains illuminated
  • TAD will remain disengaged
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16
Q

What provides power to the aileron/elevator trim system?

A

AIL/EL TRIM circuit breaker on the battery bus circuit breaker panel

17
Q

What provides power to the rudder trim system?

A

RUD TRIM circuit breaker on the battery bus circuit breaker panel

18
Q

What is the purpose of the Trim Aid Device (TAD)?

A

Assist the pilot in maintaining directional trim, reduce out-of-trim rudder forces, and maintain coordinated flight

19
Q

The computer calculates inputs to rudder trim for TAD based on what?

A
  • Pitch rate
  • Altitude
  • Airspeed
  • Engine torque
20
Q

What is required in addition to the TAD system during flight?

A

Pilot trim inputs

21
Q

What does TAD do weight on wheels and

A

Sets the rudder trim to takeoff position

22
Q

What controls the TAD system?

A

The TRIM AID switch

23
Q

What happens to the TRIM AID switch when the trim interrupt button is used?

A

It turns to the OFF position

24
Q

How would you restore TAD after using the trim interrupt switch?

A

Move the TAD switch back to TRIM AID

25
Q

What is the gust lock used for?

A

To prevent excess wear and damage to the primary flight controls

26
Q

Where is the gust lock located?

A

Front cockpit