Flight Controls Flashcards

1
Q

When will the MFSsAuto retract on GRD

A
  1. Wheel speed < 45 kts

2. TLA moved beyond 35* after landing (G/A scenario)

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2
Q

What happens when Rudder Pedals are jammed

A

Rudder Control is maintained thru the YD and Turn Coordination (FCM Function)

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3
Q

What is the path between Rudder Pedals and Rudder Surface

A

Rudder Pedals > ACE with FCM inputs > PCU > Rudder Surface

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4
Q

How do the FLT Controls operate when the RAT is the only AC Power source

A
  1. HS Trim operates at LO speed
  2. S/F system operates at LO Speed
  3. S/F Position is limited to 3
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5
Q

What is the Path from Trim to Horizontal Stablizer

A

Trim Priority > ACE with FCM Input > DC Electric TrimMotor > HSA > Horizontal Stabilzer

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6
Q

Will the MFS function in Direct Mode

A

Yes, for Roll only and at a Default Fixed Gain

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7
Q

How are the FLT Controls Trimmed

A

Roll and Yaw = Surface repositioned to a new “Neutral Position”

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8
Q

The ________ is the Communication link between the FCM’s and the P-ACE’s

A

Controller Area Network Bus (CAN BUS)

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9
Q

How are the P-ACE’s connected to the FCM’s

A

FCM’s are connected to Controller Area Network Bus (CAN BUS) to provide inputs to 3 P-ACE’s

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10
Q

Where are FCM’s 1 & 2 located

A

MAU 1 in the FWD E-Bay

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11
Q

Pitch Trim Priority

A
  1. Backup Trim
  2. CA Trim
  3. FO Trim
  4. AP Trim
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12
Q

What are High Level Functions (FCM) for the Rudder

A
  1. Yaw Damp
  2. Turn Coordination
  3. Gain on Airspeed
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13
Q

Where are the S-ACE’s (Spoilers) located

A

Located in FCM #1, FCM #3, FCM #4 which have wiring to control the S-ACE’s

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14
Q

Will Speed Brakes/Spoilers work in Direct Mode

A

NO

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15
Q

What is Max Rudder deflection

A

30* either direction

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16
Q

When do Speed Brakes 3,4,5 Auto Retract in FLT

A
  1. S/F of 2 or >
  2. Airspeed < 180 kts
  3. TLA > 70*
17
Q

How do you know if you have a FLT Control Problem

A

FLT Controls Synoptic Page (FLT Control will be Yellow)

18
Q

When will the Spoilers 1-5 Auto Deploy

A
  1. WoW
  2. Wheel Speed > 45 kts or Airspeed > 60 kts
  3. TLA < 26*
19
Q

What is Path from Control Wheel to Elevator

A

Control Wheel > ACE with FCM input > PCU > Elevator Surface

20
Q

What is Path from Control Wheel to Aileron Surface

A

Control Wheel > PCU > Aileron Surface

21
Q

What is Path from Control Wheel to S/F Surface

A

Slat/Flap lever > 2 SF-ACE > PDU > Flap Surface

22
Q

What Actuator controls Pitch Trim

A

HS-ACE Communicates with 2 DC Electric Trim Motors (Active/Standby motors) that drive the Horizontal Stabilizer Actuator (HSA)

23
Q

How long does the FBW Backup Battery last

A

15 minutes and is charged by DC ESS Bus 3

24
Q

What are 3 Higher Level Functions for Pitch Control

A
  1. Gain on Airspeed
  2. Elevator Thrust Compensation
  3. AoA Limiting
25
Q

What are some of the ways that the FLT Controls can go into Direct Mode

A
  1. Automatic detection of Channel Failure

2. Manually selected of FLT Controls Mode Panel Loss of Airspeed Data

26
Q

What happens to System logic when you go into Direct Mode

A

FCM’s are removed from the Control Loop

27
Q

Where is FCM 3 & 4 located

A

MAU 3 in Mid E-Bay

28
Q

There are how many SF-ACE’s

A

2 SF-ACE’s located in Mid E-Bay (1 for Slats, 1 for Flaps)

29
Q

How many P-ACE’s are there

A

3 Primary Actuator Control Electronics (2 FWD E-Bay, 1 AFT E-Bay) and controls Elevators and Rudders. Each has 2 Channels (Active and Standby)

30
Q

What are Secondary FLT Controls

A
  1. Horizontal Stabilizer
  2. Flaps and Slats
  3. Multi Function Spoilers (MFS)
  4. GRD Spoilers
31
Q

What happens when you Pull the Elevator Disconnect Handle

A

Isolates CA and FO Control Columns for Elevator Control

32
Q

What does Pressing one of the 3 FLT Control Mode Panel Buttons do

A

Brings the Respective FLT Control into Direct Mode

33
Q

How many ACE’s and FCM’s are there

A

9 ACE’s

4 FCM’s