Flight Control Panel Flashcards

1
Q

What does ELAC stand for?

A

Elevator Aileron Computer

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2
Q

How many ELACs are installed?

A

2

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3
Q

What are the functions of the ELAC?

A
Pitch All, Abnormal altitude, Roll normal and direct, Aileron droop, Auto pilot acquisition, Activates and protect.
Normal  elevator  and  stabilizer  control 
Normal  aileron  control 
Normal  pitch  and  roll 
Alternate  pitch 
Direct  pitch  and  roll 
Abnormal  attitude 
Aileron  droop 
Acquisition  of  autopilot  orders
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4
Q

Under Normal Law, what does ELAC 1 control

A

Primary - Aileron control (roll)
Standby - Elevator / Trimmable Horizontal Stabilizer control (backs up ELAC 2)

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5
Q

What does SEC stand for?

A

Spoiler Elevator Computer

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6
Q

How many SECs are installed?

A

3

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7
Q

What functions are performed by the SECs?

A

Pitch alternate and direct, Abnormal attitude, Roll normal and direct, Speed brakes, and Spoilers.
Normal roll (by controlling the spoilers)
Speed brakes and ground spoilers (SEC 1 & 3 only)
Alternate pitch (SEC 1 & 2 only)
Direct pitch (SEC 1 & 2)
Direct roll
Abnormal attitude

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8
Q

Under Normal Law, what do the 3 SECs control

A

Primary – Spoiler control (roll)
Standby – Elevator / Stabilizer control (SEC 1 & 2 back up the ELACs)

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9
Q

What is the sole purpose of SEC 3 in Normal Law

A

Spoiler control (Spoilers 1 & 2 only)

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10
Q

What is the definition of FAC?

A

Flight Augmentation Computer

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11
Q

How many FACs are installed?

A

2

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12
Q

What are the functions of the FACs?

A

Normal roll (turn coordination and yaw damping)
Rudder trim
Rudder travel limit
Alternate yaw

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13
Q

Under Normal Law, what do the FACs provide (YAWL)?

A

Y - Yaw Control – Damping and turn coordination, rudder limiter, rudder trim)
A - Airspeed Protection Computation (Alpha Protection, high / low limits, maneuvering speed, PFD speed scale)
W - Windshear protection (Reactive and not Predictive)
L - Low Energy Warning Protection (“SPEED, SPEED, SPEED”)

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14
Q

Is full rudder deflection available during all flight regimes?

A

No. Rudder deflection is limited as a function of airspeed

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15
Q

How are the flight control surfaces controlled and actuated?

A

All surfaces are controlled electrically and actuated hydraulically

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16
Q

When is automatic pitch trim available?

A

In flight under Normal Law with bank angle less than 33˚ with or without autopilot engaged

17
Q

How is roll control normally achieved?

A

1 aileron and 4 spoilers on each wing

18
Q

If both FACs fail, is maximum rudder deflection available?

A

Yes, after slat extension