FLT CTL Panel Flashcards

0
Q

ELACS (how many):

A

2

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1
Q

ELAC (stands for):

A

Elevator Aileron Computer

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2
Q

ELAC Functions:

A
  1. Normal Elevator & Stabilizer Control
  2. Normal Aileron Control
  3. Acquisition of Autopilot Orders
  4. ALTERNATE Pitch
  5. DIRECT Pitch & Roll
  6. ABNORMAL ATTITUDE LAW
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3
Q

ELAC 1 Normal Law:

A
  1. Primary- Aileron Control
  2. Standby- Elevator/Stabilizer Control (backs up ELAC 2)
  3. Provides 5° Aileron Droop
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4
Q

ELAC 2 Normal Law:

A
  1. Elevator/Stabilizer

2. Standby- Aileron Control (backs up ELAC 1)

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5
Q

SEC (stands for):

A

Spoiler Elevator Computer

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6
Q

SECS (how many):

A

3

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7
Q

SEC Functions:

A
  1. Normal Roll (spoilers)
  2. Flight & Ground Spoilers (SEC 1- #3 & 4, SEC 2- #5, SEC 3- #2 flight & #1+2 grnd)
    #1, 2, 3, 4, 5= Grnd
    #2, 3, 4, 5=Roll
    #2, 3, 4= Speed Brks
  3. ALTERNATE Pitch
  4. DIRECT Pitch & Roll
  5. ABNORMAL ATTITUDE LAW
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8
Q

SECS (normal law):

A
  1. Primary- Spoiler Control

2. Standby- Elevator/Stabilizer Control (SEC 1 & 2 backup of ELACS if both failed)

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9
Q

SEC 3:

A

Spoiler Control

#2 spoiler flight, #1+2 ground

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10
Q

FAC (stands for):

A

Flight Augmentation Computer

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11
Q

FAC’s (how many):

A

2

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12
Q

FAC’s Functions:

A
  1. Normal Roll (yaw dampening & turn coordination)
  2. Rudder Travel Limit
  3. Rudder Trim
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13
Q

FAC’s Provide (Normal Law):

A

-(YAWL)

1.Yaw cntrl- damping, turn coordination, limiter, trim
2. Airspeed prot computation- PFD spd scale (VLS,
VFE, mnvrng spds=GD/S/F, Alpha Prot,…)
3. Windshear Detection
4. Low Energy Warn

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14
Q

BOTH FAC’s VALID:

A
  • FAC1: Controls Yaw Damper, Turn Coordination, Rudder Limiter, Rudder Trim.
  • FAC2: Standby.
  • FAC1: Keeps aircraft within flight envelope through FD1.
  • FAC2: Performs this through FD2.
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