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
What is the gust lock used for?
To prevent excess wear and damage to the primary flight controls
26
Where is the gust lock located?
Front cockpit