Automflight Flashcards

1
Q

With the bank limit selector on the MCP in AUTO and the heading select mode engaged, bank angle
will vary from ___ to ___ degrees and is a function of true airspeed.

A

15-25

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2
Q

When using Autothrottles during an Autoland, approach speed corrections for wind are not required,
as sufficient gust protection is available with Autothrottle engaged by using Vref +5 kts.

A

Vref +5

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3
Q

Elevator, Aileron and Rudder trim can be used with autopilot engaged.

A

F

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4
Q

With a single autopilot engaged the use of electric pitch trim switches will disengage the autopilot.

A

T

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5
Q

On the ground with no autopilot engaged and FD’s off, the first FD switch turned on activates the FD
in which mode(s)?

A

Takeoff (TO) mode

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6
Q

When are the Autoland Status annunciators normally blank?

A

All normal autopilot modes except during an ILS approach below 1500 feet

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7
Q

After glide-slope capture, which of the following modes should appear on the EICAS Thrust Mode
Display?

A

Ga

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8
Q

During takeoff in the N1 mode, which of the following will cause the auto throttle system to stop
advancing the Thrust Levers?

A

Either engine reaches the takeoff N1 limit

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9
Q

During takeoff, when is the THR HOLD mode engaged?

A

80kts

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10
Q

What is the default pitch mode when an autopilot is selected to Command while in flight, with neither Flight Director on?

A

V/S

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11
Q

What is the default pitch mode when an autopilot is selected to Command while in flight, with
neither Flight Director on?

A

Climb limit N1, flap placard speeds, and Vmo/Mmo

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12
Q

What pitch commands are followed by the AFDS as a result of engaging the VNAV mode?

A

FMC commands

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13
Q

During a crosswind ILS approach, at what approximate altitude does the autopilot enter the runway
alignment mode?

A

500ft

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14
Q

approximately what radio altitude does the autopilot start the landing flare?

A

50

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15
Q

How is the autopilot flare engage mode annunciated to the pilots?

A

FLARE replacing G/S on the FMA’s

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16
Q

What is the FMA annunciation indicating the auto throttle system is retarding the Thrust Levers
during the landing flare?

A

Idle

17
Q

What annunciation change occurs when the Approach mode is selected?

A

LOC and G/S armed (white) appear in the FMA

18
Q

How can the crew get the localizer and glideslope deviation scales displayed on the ADI’s?

A

Select an ILS frequency on the ILS tuning head

19
Q

When go-around mode is engaged, the auto throttle:

A

Adjusts thrust to maintain 2,000 fpm climb

20
Q

When does the Go-Around mode arm for the AFDS and auto throttle system?

A

Gs capture

21
Q

In order for LAND 3 to be active, which of the following events must have occurred?

A

RA must be 1500’ or less and GS and LOC must be captured.

22
Q

When the Go-Around mode is deactivated, which autopilot will remain engaged?

A

First in command

23
Q

Which controls do the autopilots use to track the localizer in the ROLLOUT Mode?

A

Rudder and nose wheel steering

24
Q

During an ILS approach, below which approximate altitude is the Go-Around mode inhibited?

A

5 feet radio altitude for more than 2 seconds

25
Q

After landing, which one of the following is required to disengage the operating AFDS mode?

A

Disengage all autopilots and turn off both flight directors

26
Q

How can you de-select the Approach Mode AFTER localizer and glide-slope captured

A

Select GA Switch or Autopilot off and both Flight Directors OFF then ON

27
Q

How can you disarm, LNAV, LOC, VNAV and APP modes when armed and prior to capture?

A

Push the mode switch a second time

28
Q

What pitch is commanded by the AFDS when GA is selected in a windshear recovery on approach?

A

15 degrees pitch-up or slightly below the pitch limit, whichever is lower

29
Q

Describe the condition that would cause VNAV ALT to display as the pitch mod

A

A conflict occurs between the VNAV profile and MCP altitude

30
Q

If in level flight with both flight directors off, which pitch and roll modes will the autopilot engage in if commanded on?

A

Vertical Speed (V/S) and Heading Hold (HDG HOLD)

31
Q

After takeoff, when may the autopilot be engaged?

A

After a pitch mode is selected

32
Q

When does the ALT light on each altimeter illuminate?

A

Between 300’ and 900’ of the MCP Altitude

33
Q

What does the THR HOLD mode indicate?

A

Power is removed from the auto throttle servo system

34
Q

How is rollout mode engagement annunciated?

A

Rollout appears on the FMA’s in green