Automatic Flight Flashcards

1
Q

What display unit do Flight Mode Annunciations (FMA)

appear on?

A

Primary Flight Display (PFD)

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2
Q

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

A

One or both autopilots engaged.

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3
Q

The Flight Mode Annunciator (FMA) displays a rectangle

around each mode annunciation _____.

A

for 10 seconds after mode engagement

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4
Q

The FMA displays Armed Modes in ____ at the bottom of

the flight mode annunciation boxes.

A

small white letters

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5
Q

The Flight Mode Annunciators (FMA) displayed on the

Primary Flight Display (PFD) are (from left to right):

A

autothrottle; roll; pitch

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6
Q

Which FMA indicates that power has been removed from

the autothrottle servos during takeoff?

A

THR HLD

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7
Q

Pushing an illuminated mode switch (other than APP mode after capture) on the Mode Control Panel (MCP) _____ the mode.

A

deselects

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8
Q

Turning a Flight Director (F/D) switch ON displays command bars on the respective pilot’s attitude indicator if _____ and _____ modes are engaged.

A

command pitch / roll

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9
Q

The master FCC”,” with no A/Ps engaged in CMD”,” is the

______.

A

FCC for the first F/D turned on

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10
Q

The requirements for A/P engagement are ______.

A

Correct Answer 4

1) no force applied to control wheel
2) select either CMD and/or CWS switch on MCP
3) STAB TRIM AUTOPILOT cutout switch is NORMAL
4) all of the above

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11
Q

The STAB OUT OF TRIM (amber) light indicates the _____.

A

A/P is not trimming the stab properly”,” and the A/P

remains engaged

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12
Q

The A/P Disengage Light illuminates STEADY RED for _____. (Select ALL correct answers)

A

Correct Answer 2, 3
1) anytime the A/P disengages
2) the stabilizer out of trim below 800 ft RA on dual
channel approach
3) the ALT ACQ mode inhibited during A/P go-around if the
stabilizer is not trimmed for single A/P operation
4) a visual verification of CWS

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13
Q

The ____ indication (white) on the Upper Display Unit
means the FMC is not providing the Autothrottle system
with N1 limit values.

A

A/T LIM

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14
Q

The MCP IAS/MACH display is blank _____.

A

Correct Answer 4

1) with VNAV mode engaged
2) with A/T engaged in FMC SPD mode
3) during 2 engine AFDS go-around
4) all of the above

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15
Q

While flying an RNP departure passing 10,000’”,” you have selected LVL CHG”,” with 250 in the IAS/MACH window on the MCP”,” what will be the Pitch Mode FMA annunciation?

A

MCP SPD and the airplane will fly 250 knots as shown on the MCP

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16
Q

How is the MCP IAS/MACH display manually changed

between indicated airspeed and Mach number?

A

By pressing the C/O (change over) switch on the MCP.

17
Q

The Bank Angle Selector (rotating knob) sets maximum bank angle for AFDS operation in which Roll modes

A

HDG SEL or VOR

18
Q

Engaging LNAV outside of 3 NM from an active route

requires an intercept course of _____ degrees or less and to intercept a route segment _____ an active waypoint.

A

90 / before

19
Q

After engaging LVL CHG for a climb”,” what does the FMA

annunciate for the Autothrottle mode?

A

N1

20
Q

After localizer and glide slope capture”,” disengage APP

mode by ______.

A
Correct Answer 4
1) pushing a TO/GA switch
2) retuning the VHF NAV receiver
3) disengaging autopilot(s) and turning off both F/D
switches
4) any of the above
21
Q

The aircraft is climbing from 10000’ to FL200 in VNAV with 20000’ selected in the FMC CRZ page and MCP Altitude window. Passing through 11000’”,” if ALT HLD is selected”,” the aircraft will ______.

A

stop climb and level off at 11000’

22
Q

Activating either TO/GA switch above 2000’ RA with flaps up and G/S not engaged results in ______.

A

nothing

23
Q

Glide Slope capture is inhibited: ______.

A

prior to localizer capture

24
Q

After pushing TO/GA once on a dual A/P approach prior to touchdown”,” the roll mode commands _____.

A

current ground track

25
Q

After pushing TO/GA once on a dual A/P approach prior to touchdown”,” the autothrottle provides thrust for _____.

A

1000-2000 fpm climb

26
Q

On a go-around with A/T engaged”,” the second push of
TO/GA (after A/T reaches the reduced go-around thrust)
causes the A/T to _______.

A

advance to the full go-around N1 limit

27
Q

Overspeed or underspeed limiting symbols appear in the

MCP speed window when _______.

A

the commanded speed cannot be achieved (too fast or

too slow)

28
Q

When deviating 200 feet from the selected altitude”,” the
Deviation Alerting System sounds a momentary tone and
_____.

A

the current altitude box turns amber and begins to flash