Flight Control Questions Flashcards

1
Q

What is the only primary flight control that is not FBW (fly-by-wire)

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 speed
  • 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
  • Back-up
  • Captain
  • First officer
  • Autopilot
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6
Q

How is roll controlled?

A
  • Ailerons and multifunction spoilers (outer 3 spoilers on each wing)
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7
Q

How many spoiler are on each wing? What are their functions?

A
  • 5
  • 3 outboard multifunction spoilers are used to assist in roll control, as speed brakes, and as ground spoilers
  • 2 inboard spoilers are only used as ground spoilers
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8
Q

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

A
  • Slat/flaps selected to 2 or greater
  • Airspeed < 180 its
  • TLA > 70
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9
Q

What is the flap/slat 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 fell if flight controls are disconnected?

A
  • Artificial feel is felt at 1/2 the normal load
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13
Q

How are the flight controls trimmed?

A
  • Roll & Yaw ailerons and rudder surface repositioned to a new neutral position
  • Pitch horizontal stabilizer
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14
Q

Will the multifunction spoilers function in DIRECT mode?

A

Yes, for roll only and a default fixed gain

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15
Q

Will the speed brake/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 tim operates at LO SPEED
  • Slat/Flap system operates at LO SPEED
  • Slat/Flap position is limited to 3 to allow adequate airspeed for the RAT