AFCS

There are ____ FCCS which process________

2, attitude information

2, attitude and AHRS or IRS information and ADC information

3, attitude and AHRS or IRS information and ADC information

4, heading information

On FCP, lamps light on each side of a mode push button indicates

That mode has captured

That FCC 1 and/or FCC 2 hace acknowledged that mode input

That mode is armed

The autopilot is on

If a new flight director mode becomes active, the annunciator in the FMA will

Flash green for 5 seconds the steady

Flash white 10 times the steady

Flash yellow then green

Flash red then green

Pressing either go-around ( TOGA) switch on a thrust lever will

Discoteca the autopilot

Engage the autopilot in go-around mode

Automatically advance thru levers to take-off thrus

Disengage the flight Director

When the Pilots flight director fails and not the co-pilot , it is announced with a _____ message on EICAS

White FD 2 FAIL

Red AFCS MSGS FAIL

White FD 1 FAIL

None of the above

During flight with autopilot on (engaged) .Select the true statement

Pressing the onside FD pushbutton has no effect on the coupled FD or autopilot

Pressing the onside FD pushbutton will remove the FD from both PFD

Pressing the onside FD pushbutton will remove the FD from onside PFD

Pressing the offside FD pushbutton will remove the FD from offside PFD

Glideslope can only be captured when

Approach mode selected

Inbound

With a valid localizer as the lateral navigation source

All of the above

With the flight director in take-off mode, the vertical aspect of the command bars will:

Pith up to a fixed 10 deg angle

Pith to a lower angle with the loss of an engine

Have an initial 9 pitch attitude and when airborne a variable pith up angle with engines operating

Both b and c are correct

When both engines are available, the vertical take-off mode generates a ____ degree pith-up command

Initially a fixed pith value and once airborne a variable pith attitude

There is no indication until gear up

The automatic mode transition to half bank will occur at _____ feet

31,600

27,400

29,350

32,200

Above what altitude will half bank mode be selected automatically?

15,000

31,000

31,600

27,400

Pressing the SPEED button on the FCP twice will

Select DES mode

Select IAS mode

Select CLB mode

Deselect speed mode

Half bank mode reduces the maximum commanded bank angle to ____ degrees

The AFCS receives sensors information from

The AIr data system

Navigation system

Radio Altimeter

All of the above

In order to engage the autopilot, Which of the following conditions must exist?

At least one yaw damper must be engaged

Both FCCS must be operative

Both AHRS/IRS and one ADC must be operative

All of the above

Of the following, with will disconnect the autopilot?

Activating the stab trim swiches

Pressing the AP ENG button on the FCP

Pressing the YD DISC button

All of the above

Select one way which the autopilot can be manually disengaged.

By manually moving either control wheel in pitch or roll

When yaw damper system fails

By activating the stab trim swiches on the control wheel

During wind shear avoidance procedures

From the list below identify the 4 lateral modes of the flight director .1 Speed 2Approach 3 Heading 4 Altitude 5 Vertical speed 6 Navigation 7. 1/2 bank

2,3,6,7

2,4,5,6

1,3,5,7

1,2,3,6

With the XFER pushbutton on the FCP panel selected:

Flight director 1 is the active system and the co-pilot has control of both flight director modes

Flight director 1 is disables and flight director 2 needs to be selected by either pilot

Autopilot is engaged and both flight directors are inactive

Flight director 2 is used ad the active flight director

The CRJ100 aircraft is equipped with two independent flight directors which provides

Manual input to the automatic flight control system for pitch and heading commands only

Flight guidance in the event of loss of all DC power

Selectable company routes information from database

Flight guidance commands to the autopilot and steering commands of the pilot when the aircraft is hand flown

Turbulence mode cannot be selected if

The automatic pitch trim is engaged

The on-side localizer is captured

The autopilot is disengaged

Both b and C

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