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Billy 190 Systems > Flight Controls > Flashcards

Flight Controls Flashcards

1
Q

Elevators, rudders, and roll spoilers as well as the secondary flight control systems are controlled by ____
technology.

A

Fly-by-Wire (FBW)

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2
Q

Direct mode of operation is primarily the result of loss of data from all ____ (no airspeed input) or multiple ____
failures.

A

FCMs; ACEs

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3
Q

The electrical PBIT test is automatically performed during power up and takes approximately ____ minutes.

A

3 minutes

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4
Q

Manual trim is activated by

A

Both A and B(Switches on each control column, A standby switch located on the main pedestal)

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5
Q

In case of an electrical failure, followed by RAT deployment, the trim function will operate at____ for either manual mode trim or autopilot trim.

A

Low Rate

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6
Q

Aileron control is accomplished through___

A

a conventional cable system

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7
Q

Rudder trim function is limited to ____ seconds. If further displacement of the trim system is required the command must be released and reapplied.

A

3

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8
Q

When the RAT is the only source of electrical power, the SF-ACE will prevent the slats and flap beyond position
____

A

3

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9
Q

After touchdown, the FCM will command all multifunction spoiler surfaces to extend 40° and the ground spoiler surfaces to 60° when

A 
All of the above (Weight on wheels, Wheel speed is above 45 kts. or airspeed is above 60 KIAS, Thrust
Lever Angle (TLA) below 26°)
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10
Q

The speed brakes will automatically retract when the

Flap/Slats 2 or greater or airspeed is decreased below

A

180 KIAS

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11
Q

Flap/Slat position 4 is gated for

A

Go-around and take-off

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12
Q

Position 5 and FULL are used

A

Landing

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13
Q

The flight controls synoptic page provides a visual representation of the flight control system operation and parameters, and can be selected by the flight crew for viewing on either ____

A

MFD

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14
Q

Which flight controls are not fly by wire?

A

Ailerons

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15
Q

Describe the function of the RED AP/TRIM disconnect button on the Control Wheel.

A

Disconnects the Autopilot and interrupts all trim inputs

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16
Q

Which Pitch Trim switches have priority?

A

The captain has priority over the first officer

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17
Q

What is the function of the guarded FLIGHT CONTROL MODE pushbuttons when pushed in?

A

To enable Direct mode

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18
Q

What is the difference in flaps and slats between the FLAP 4 and 5 lever position?

A

No physical difference, flap 4 is gated for takeoff go around logic where flap 5 is for landing logic

19
Q

Are speed brakes available in DIRECT MODE?

A

Multi-Function Spoiler system is only available to assist in roll augmentation

20
Q

On the EICAS Slat/Flap/SPDBRK indication what does the single green boxed number represent?

A

Displays the SLAT/FLAP surface position

21
Q

In the case of surface jamming, what will be different about the boxed display?

A

An additional box will be displayed in Amber

22
Q

How long can the manual pitch trim switches be split before a lockout of the respective trim switches occurs?

A

7 seconds

23
Q

What is the purpose of the PITCH Trim SYS 1 and 2 CUTOUT Buttons when pushed out?

A

Disables the respective HS-ACE channel

24
Q

Will the autopilot directly operate the Horizontal Stabilizer trim system when the autopilot is engaged?

A

Yes through the HS-ACE

25
Q

What primary flight control system/s is not Fly By Wire?

A

Ailerons

26
Q

What primary flight control system/s is Fly By Wire?

A

All flight controls are fly by wire except ailerons

27
Q

With only hydraulic system 3 pressurized/working, what primary flight control/s are capable of working?

A

Ailerons, Elevator and Rudder

28
Q

What is the power source for Slats?

A

Electric

29
Q

What is the power source for Flaps?

A

Electric

30
Q

How many Multi-Function Flight Spoilers are on each wing?

A

3

31
Q

How many Ground Spoilers are on each wing?

A

2

32
Q

What flight controls are Anti-iced?

A

Slats (3 per wing) outboard of Engine

33
Q

What is the power source for moving the Horizontal Stabilizer?

A

Electrical

34
Q

When is the Horizontal Stabilizer set for takeoff?

A

When load close out received

35
Q

What is the default flap setting for takeoff?

A

2

36
Q

If other than a flap 2 setting is to be used for takeoff, does this new flap setting need to be updated anywhere else?

A

Must be changed on MCDU TAKEOFF pg. 2

37
Q

What primary flight controls work when all Hydraulic systems have failed?

A

None

38
Q

What is referenced when doing a Flight Control Check?

A

FO’s MFD Systems FltCtrl screen

39
Q

Where do you view what the Horizontal Stabilizer Trim is set to?

A

Engine EICAS screen

40
Q

If the autopilot is engaged and pitch trim is actuated, what will happen to the autopilot?

A

Autopilot disengages

41
Q

During a flight control check, what are you looking for?

A

Solid Green Box or Green boarder box with green diagonals

42
Q

Prior to doing a flight control check what must be checked?

A

No Amber boxes in the STATUS area on the MFD Systems FltCtrl page

43
Q

What is the purpose of the Elevator Disconnect Handle?

A

Isolates the Captains and FO’s control columns for control of a non-jammed elevator

44
Q

What is the purpose of the Aileron Disconnect Handle?

A

Isolates the Captains and FO’s control wheels for control of a non-jammed aileron

Billy 190 Systems (15 decks)

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