Auto Flight Flashcards

1
Q

What systems make up the Automatic Flight Control System (AFCS)

A

1) The flight director (FD)
2) Autopilot (AP)
3) Auto-throttles (AT)

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2
Q

Which panel hosts the controls for the AP, AT and FD, plus lateral and vertical reference/ mode selection

A

The Automatic Flight Control System Panel

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3
Q

What does pushing the FD button on the AFCS panel do?

A

Engages and disengages the flight director on those PFDs

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4
Q

What does pushing the AT button on the AFCS panel do

A

Engages and disengages the Auto-throttle

Selects the source of the speed reference between MAN and FMS

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5
Q

What does pushing the HDG button on the AFCS panel do

A

Selects heading mode when pushed once and roll mode when pushed again.

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6
Q

Pushing the BANK button on the AFCS will toggle between what bank angles

A

+- 15 deg and +- 30 deg

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7
Q

What is the up and down range of the FPA mode

A

9.9 deg up and down

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8
Q

How can the flight patch angle/ reference line be selected?

A

By rotating the FPA knob

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9
Q

What does the outer knob of the ALT knob select? The inner knob?

A

1) Outer - Selects the altitude increasing/decreasing 1000 feet.
2) Inner - Selects altitude increasing/ decreasing 100 feet

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10
Q

What does pushing SRC button do

A

Alternates between PFD 1 and PFD FMA modes as the source for the auto pilot

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11
Q

When the autopilot is engaged, what does pushing the TCS button on the sidestick do

A

It activates the TCS (AP override) as long as neither the takeoff or go around mode is active.

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12
Q

Where are the AT/DISC buttons located? The TO/GA buttons

A

On the Thrust levers

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13
Q

With the AP engaged, will the AP disengage if the force is applied on the sidestick, either in the pitch or roll direction.

A

Yes

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14
Q

What are the two FD cues presented?

A

The flight director cue (magenta circle) and the takeoff cross bar.

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15
Q

What does the green Flight Patch Vector cue indicate?

A

The current flight patch in reference to the horizon line.

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16
Q

Where is the Flight Mode Annunciator (FMA) located and what does it display

A

On the upper part of both PFD’s and it provides annunciation for auto throttle, autopilot, approach status, lateral and vertical modes.

17
Q

List the FMA color codes for normal operation

A

1) Magenta - For FMS active/ engaged modes
2) Green - Non- FMS active/ engaged modes
3) White - Armed modes
4) Red - Abnormal condition.

18
Q

What does the amber LIM on the FMA indicate

A

The autothrottle is in speed mode and the selected speed mode and the selected speed target cannot be achieved because the auto throttle has limited N1

19
Q

What are the two precision approach capabilities of the airplane

A

Either APPR 1 or APPR 2

20
Q

When is the AP aural alert triggered

A

When the AP is disengaged due to a system failure

21
Q

How can the AP aural alert be cancelled.

A

By pressing the AP/PTY buttons on either side stick

22
Q

When will the airplane automatically transition to the half bank mode

A

When the aircraft altitude is greater than 25,000 feet during a climb.

23
Q

Prior to selecting the TOGA button what must be set in order to display the TO crossbar on the PFD

A

Flaps must be set to 1 or 2, aircraft weight must be set and TO speeds must be sent to the FMS

24
Q

What computed takeoff speed reference is set in the TO mode

A

V2+15kts (AEO), in the case of OEI below V2 the speed reference will be set to V2

25
Q

What altitudes are associated with the ILS approach check points to try to engage the highest system capability available

A

1500 ft RA and 800 ft RA

26
Q

What is emergency descent mode (EDM)

A

A function that can automatically bring the airplane to a safe altitude in the scenario of cabin depressurization and pilot incapacitation.

27
Q

When is EDM enabled

A

When EDM is enabled and a depressurization event occurs (a red cabin altitude CAS message is displayed).

28
Q

If the AP is engaged, what happens to the AT when the Airspeed is below the LSA white bar.

A

The AT will automatically be engaged.

29
Q

What happens to the AP when the AOA limit function is activated.

A

It is disengaged.

30
Q

What phases of flight is the AT system approved to operate in

A

All phases of flight, takeoff, climb, cruise, descent, approach, landing and during OEI operations.

31
Q

What is the purpose of the hold mode of the AT

A

To ensure that no undesirable thrust reductions are experienced during TO

32
Q

When will the AT hold mode be activated

A

From the time the airplane exceeds 60 kts during the TO roll until 400 ft AGL.