Autoflight Flashcards

1
Q

What does a flashing 8 mean in the airspeed window?

A

Selected speed is greater than the over speed limit

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2
Q

What does a flashing A mean in the speed window?

A

Selected speed is less than the minimum speed

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3
Q

The speed control on the MCP automatically changes to Mach above what altitude?

A

26,000 ft

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4
Q

What does a lit up button on the MCP mean?

A

That the mode can be deselected.
It does NOT mean a specific mode is active.

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5
Q

After the APP light extinguished on an approach, how can the APP mode be disengaged?

A

Pushing TOGA

Disengaging the autopilot by turning off both FDs

Selecting a different frequency in one of the VHF Nav receivers

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6
Q

The autothrottle servos are de-energized in what two modes? Allowing the pilot to manually adjust thrust lever position

A

THR HOLD

ARM

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7
Q

What does a white A/T LIMIT above the engine N1 indicators mean?

A

The FMC is not providing limits to the autothrottle system

Or

The system is using a degraded N1 thirst limit from the EEC

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8
Q

The three columns on the FMA represent what? (In order L to R)

A

Auto throttle mode
Roll mode
Pitch mode

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9
Q

What does FD indicate on the AFDS?

A

That the flight director is turned on, but the autopilot is either off or in CWS mode

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10
Q

What does an amber CWS R or CWS P in amber below the FMA mean?

A

Control wheel steering is engaged in the roll or pitch mode respectively

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11
Q

MA (master) displays above which flight director?

A

Which ever is selected in first (with no autopilot engaged)

Which ever FCC is controlling the autopilot (autopilot on)

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12
Q

An amber FD displayed on the PFD means what?

A

There is a fault in the FD system. Command bars should also be missing

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13
Q

Flight control computer A/B is selected for use how?

A

Whichever autopilot master is turned on first

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14
Q

Minimum altitude for autopilot engagement?

A

1000 ft AGL

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15
Q

What happens if you press/disengage an active autopilot mode?

A

The aircraft reverts to CWS in that mode (pitch/roll), CWS P/R illuminates on the PFD, A/P disengage light flashes amber, that pitch or roll mode must be manually controlled

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16
Q

A/P engagement is only allowed if two pilot controlled conditions are met, what are they?

A

No force is being applied to the control wheel

Stabilizer trim AUTOPILOT cutout switch is in the NORMAL position

17
Q

What happens if you press the other autopilot CMD switch while an autopilot is active?

A

The autopilot simply transfers to the other FCC. No disengagement occurs

18
Q

T/F: Aileron trim can bd used with the autopilot engaged

A

FALSE
THE USE OF AILERON TRIM IS PROHIBITED ANY TIME THE AUTOPILOT IS ENGAGED

19
Q

What are all the ways to disengage the autopilot?

A

Pushing the autopilot disconnect on the control wheel or MCP (bar down)

Pushing the illuminated CMD mode on the MCP

Activating either pilots control wheel trim switch

Moving the STAB TRIM AUTOPILOT cutout switch to CUTOUT

Pushing TOGA with AP engaged below 2,000 ft RA

Pushing TOGA with AP engaged above 2,000 ft RA with flaps not UP or G/S engaged

20
Q

What four failures cause autopilot disengagement?

A

Either L or R IRU fails (fault light illuminates)

The respective hydraulic system pressure is lost

Loss of electrical power

Loss of a sensor input which prevents proper autopilot operation

21
Q

A/P disengage light illuminates steady red for what two conditions?

A

Altitude acquire mode inhibited during A/P go around if not trimmed for single A/P operation

When the disengage light test switch is held in position 2, or when the automatic ground system test fails

22
Q

What does the STAB OUT OF TRIM light mean?

A

Autopilot is not trimming the stabilizer properly. Only can illuminate when the autopilot is engaged

23
Q

During takeoff at ___ kts the auto throttle switches from ____ mode to ____ mode. This does what to the autothrottles?

A

84 kts
N1 mode to THR HLD mode
This disengages the servos and the crew can manually adjust the thrust levers if needed

24
Q

As the autothrottles reduce thrust for an idle descent, ____ is displayed on the FMA.

Once the thrust levers reach the idle position ____ replaces ____ on the FMA.

A

RETARD

ARM replaces RETARD

25
Q

When you press the TOGA button for a go around once, what happens? Twice?

A

First press commands a reduced thrust go around to achieve between 1,000-2,000 ft/min climb.

The second ores commands a max thrust go around

26
Q

Section 7

A

Start here