Automatic Flight System Flashcards

1
Q

What are the 3 flight mode annunciators?

A

Autothrottle, Roll, & Pitch.

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2
Q

What does CMD (green), annunciated on the PFD, mean?

A

One or both autopilots are engaged.

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3
Q

When does a rectangle around a Flight Mode Annunciator (FMA) appear?

A

When a mode changes.

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4
Q

How does an FMA display an Armed Mode?

A

Shown in smaller white letters at the bottom of the flight mode annunciation boxes.

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5
Q

What FMA annunciation indicates that power has been removed from the autothrottle servos during takeoff?

A

THR HLD

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6
Q

Pushing an illuminated mode switch on the Mode Control Panel (MCP) does what to the mode?

A

Indicates the mode can be deselected by pushing the switch.

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7
Q

What is displayed by turning a Flight Director (F/D) switch ON?

A

Turning a F/D switch ON displays command bars on the respective pilot’s attitude indicator if command pitch and roll modes are engaged.

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8
Q

How is the master FCC determined?

A

Is determined by the first F/D switch being turned on with no autopilot or coupled with the first engaged autopilot.

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9
Q

What are the required conditions for A/P engagement?

A

No force is being applied to the control wheel & the STAB TRIM AUTOPILOT cutout switch is at NORMAL.

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10
Q

What does the STAB OUT OF TRIM (amber) light indicate?

A

Autopilot is not trimming the stabilizer properly.

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11
Q

When does the A/P Disengage Light illuminate STEADY RED?

A

Stabilizer out of trim below 800 ft RA on dual channel approach, ALT ACQ mode inhibited during A/P go-around if stabilizer not trimmed for single A/P operation, disengage light TEST switch held in position 2, or automatic ground system tests fail.

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12
Q

What does the A/T LIM indication (white) on the Upper Display Unit mean?

A

Indicates the FMC is not providing the A/T system with N1 limit values.

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13
Q

When is the MCP IAS/MACH display blank?

A

VNAV mode engaged, A/T engaged in FMC SPD mode, or during 2 engine AFDS go-around.

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14
Q

What triggers/causes the MCP IAS/MACH display to automatically and manually switch between indicated airspeed and Mach number?

A

Automatic changeover occurs at approximately FL260. Manual changeover can be initiated by pressing the C/O switch.

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15
Q

The Bank Angle Selector sets maximum bank angle for AFDS operation in which Roll modes?

A

HDG SEL or VOR modes.

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16
Q

Engaging LNAV outside of 3 NM from an active route requires what intercept criteria?

A

Be on an intercept course of 90° or less & intercept route segment before active waypoint.

17
Q

After engaging LVL CHG for a climb, what does the FMA annunciates for the Autothrottle mode?

A

N1 for climb and RETARD followed by ARM for descent.

18
Q

After localizer and glide slope capture, what will exit the APP mode?

A

Pushing a TO/GA switch, disengaging A/P and turning off both F/D switches, or retuning a VHF NAV receiver.

19
Q

What will happen after activating either TO/GA switch above 2,000’ RA with flaps up and G/S not active?

A

Nothing.

20
Q

When is Glide Slope capture inhibited?

A

Prior to Localizer capture.

21
Q

After pushing TO/GA once, on a dual A/P approach prior to touchdown, what will the roll mode command?

A

Roll Mode annunciation on the FMA is blank (Current Track)

22
Q

After pushing TO/GA once, on a dual A/P approach prior to touchdown, what rate of climb will the N1 thrust provide?

A

1000 to 2000 fpm rate of climb.

23
Q

With the second push of TO/GA, on a dual A/P approach prior to touchdown, what N1 thrust is commanded?

A

Full go-around N1 limit.

24
Q

When will overspeed or underspeed limiting symbols appear in the MCP speed window?

A

When the commanded speed cannot be reached.

25
Q

What type of deviation alerting is available when deviating from the selected altitude?

A

Momentary tone sounds and the current altitude box turns amber and begins to flash.