Flight Controls Flashcards

1
Q

What is the only primary flight control that is not FBW?

A

Ailerons

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2
Q

What is the difference between normal mode and direct mode?

A

There are no higher level functions available in direct mode

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3
Q

What are the higher level functions associated with pitch?

A
  • Gain on airspeed
  • Elevator thrust compensation
  • AOA limiting
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4
Q

What are the higher level functions associated with yaw?

A
  • Yaw damp
  • Turn coordination
  • Gain on airspeed - as airspeed increases, rudder deflection decreases
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5
Q

What is the priority for the trim system?

A
  • Backup
  • Captain
  • FO
  • Autopilot
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6
Q

How is roll controlled?

A

Ailerons and multifunction spoilers (outer spoilers on each wing)

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7
Q

How many multifunction spoilers are on each wing? What are their functions?

A
  • 5
  • 3 outboard spoilers are used to assist in roll control and for ground spoilers
  • 2 inboard spoilers are ground-only
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8
Q

When will the speed brakes automatically close even if the lever shows deployed?

A
  • Flaps >= 2
  • Airspeed , 180 kts
  • TLA > 70 deg
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9
Q

What is the slat/flap extension/retraction sequence?

A

Slats extend first, flaps retract first

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10
Q

Will loss of airspeed data cause the flight controls to go into DIRECT mode?

A

Yes

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11
Q

Can a FCM override pilot input?

A

No, the pilot always has supreme control

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12
Q

What happens to artificial feel if flight controls are disconnected?

A
  • Elevator- artificial feel is felt at 1/2 normal load

- Ailerons: Captain has normal feel, FO has no feel

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13
Q

How are the flight controls timed?

A
  • Roll and yaw: Ailerons and rudder surfaces repositioned to a new ‘neutral position’
  • Pitch: Horizontal stabilizer
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14
Q

Will the multi-function spoilers function in DIRECT mode?

A

Yes, for roll only and at a default sized gain

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15
Q

Will the speed brakes/ground spoilers function in DIRECT mode?

A

No

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16
Q

What happens to the flight control system when the RAT is the only AC power source?

A
  • Horizontal stab trim operates at 1/2 speed
  • Slat/flaps system operates at 1/2 speed
  • Slat/flap position is limited to ‘3’ to allow adequate airspeed for the RAT
17
Q

What type of flaps are on the aircraft?

A

Double slotted fielder flaps, 2 per wing, 4 total

18
Q

What is the actuator the moves the slats and flaps? How are they powered?

A

PDU, power driver unit, electrically powered

19
Q

What is the actuator that moves the rudder? How is it actuated?

A

PCU, power control unit, hydraulically actuated

20
Q

What is the device that actuates the ailerons? How is it actuated and controlled?

A

PCU, power control unit, hydraulically actuated, controlled by conventional cables

21
Q

What is the device that moves the horizontal stabilizer? How is it powered?

A

HSA, horizontal stabilizer actuator, electrically powered