Autoflight

Question 1

What does the FMC provide?

Answer 1

N1 limits and target N1 for the autothrottles and command airspeeds for autothrottles and AFDS

Question 2

The AFDS is a dual system consisting of 2_____ and a single ______.

Answer 2

FCCs; MCP

Question 3

How can AFDS mode be disengaged?

Answer 3

selecting another command mode or by disengaging the autopilot and turning the FDs off.

Question 4

How can you engage the autopilot?

Answer 4

pushing a separate CMD or CWS engage.

Question 5

How is autopilot engagement in CMD or CWS inhibited?

Answer 5

force is being aplied to the control wheel or the STAB TRIM AUTOPILOT CUTOUT switch is not in normal.

Question 6

2 autopilots can be engaged at the same time unless?

Answer 6

approach mode is used.

Question 7

Dual autopilot operation provides what?

Answer 7

control through landing flare and touchdown or automatic go around.

Question 8

T/F: In single autopilot operation, full auto flare and touchdown capability and autopilot go around are available.

Answer 8

False.

Question 9

How can you disengage the autopilot?

Answer 9

push autopilot disengage switch, pushing either TOGA switch w/ a single AP engaged in CWS or CMD; below 2000’ RA or with flaps not up or glideslope engaged; pushing either TOGA switch with a single AP engaged in CWS or CMD above 2000 FA with flaps not up or glideslope engaged. Pushing either TOGA switch after touchdown with both APs engaged in CMD. Pushing an illuminated engage switch. Pushing the AP disengage bar down. Activating either pilots control wheel switch. Moving the STAB TRIM AUTOPILOT CUTOUT switch to CUTOUT. Either L or R IRS system FAULT light are illuminated. Loss of electrical power or a sensor input which prevents proper operation of the engaged autopilot and mode. Loss of hyraulic system pressure.

Question 10

Dual channel autopilot operation is possible only when ____ generators are powering the busses.

Answer 10

2

Question 11

How many RAs are there?

Answer 11

2

Question 12

With one RA inop, the autopilot will disconnect 2 seconds after ____ and ____ capture

Answer 12

LOC; Glideslope

Question 13

T/F: Command pitch and roll modes must be engaged for the FD to show.

Answer 13

True.

Question 14

FD commands are the same as Autopilot except:

Answer 14

T/O mode is a flight director mode only
Dual FD guidance is availble for single eng ops
FD has no landing flare capability

Question 15

FD command bars retract from view at ~ ______ on an ILS approach

Answer 15

50 feet RA

Question 16

With both FD switches on, the logic for both pilots FD modes is controlled by the _______.

Answer 16

Master FCC.

Question 17

Master FCC logic

Answer 17

1. With neither AP engaged, the FCC for 1st FD turned on is Master (MA)
2. With 1 or both APs engaged in CMD, the FCC for the first AP in CMD is the master FCC, regardless of which FD is on first.

Question 18

How can you tell the FDs are in independent mode?

Answer 18

Both MA lights are on in the MCP.

Question 19

If a generator fails during a FD TO or GA or while in Dual FD approach mode below 800’, the FCC on the unaffected side positions the FD on which side?

Answer 19

both sides.

Question 20

What does FD mean above the ADI?

Answer 20

FD is on and the AP is either OFF or in CWS.

Question 21

What does CWS P mean?

Answer 21

pitch mode is engaged in CWS mode

Question 22

What does CWS R mean?

Answer 22

the roll mode is engaged in CWS.

Question 23

What does SINGLE CH mean?

Answer 23

annunciated for single AP ILS approaches. It appears after Localizer capture.

Question 24

What happens when you push CWS on the MCP?

Answer 24

engages AP in pitch and roll axes and displays CWS P and CWS R on FMAs.

Question 25

If in CWS mode, when you release control pressure, what happens?

Answer 25

the AP holds existing attitude.

Question 26

If in CWS mode and aileron pressure is released within 6 degrees or less bank, the AP rolls ____________.

Answer 26

wings level and holds existing heading.

Question 27

Heading hold feature-bank

Answer 27

below 1500 FA with gear down after FD VOR capture with TAS 250 kts or less after FD LOC capture in APP mode

Question 28

How can you tell that a mode is armed in the FMA boxes

Answer 28

Smaller white letters underneath the larger green letters.

Question 29

What does GA signify?

Answer 29

ATS maintain thrust at reduced GA setting

Question 30

When you see RETARD, what do you know?

Answer 30

The ATS are moving to the aft stop and then you will see ARM mode.

Question 31

What does a white ARM mean?

Answer 31

no ATS mode is engaged. thrust lever servos are inhibited. Pilot can set thrust levers manually. Minimum speed protection is provided.

Question 32

How do you arm TOGA for takeoff?

Answer 32

both FD switches on and pushing either TOGA switch.

Question 33

How is pitch shown on FDs on takeoff?

Answer 33

10° nose down until 60 KIAS 15° nose up after 60 KIAS 15° nose up after lift off until a sufficient climb rate is acquired During climb: maintain MCP speed plus 20 kts.

Question 34

How can TOGA be engaged w/out FDs engaged?

Answer 34

TOGA pressed after 80 KIAS below 2000 AGL and prior to 150 seconds after lift off.

Question 35

TOGA is engaged for go around how?

Answer 35

inflight below 2000 RA inflight above 2000 RA with flaps not up or G/S captured not in TO mode; either FD switch ON or OFF.

Question 36

VNAV SPD vs VNAV PATH?

Answer 36

VNAV SPD: AFDS maintains FMS speed displayed on the airspeed indicator and/or CDU CLIMB or DESCENT page. VNAV PATH: AFDS maintains FMC alt or descent path with pitch commands.

Question 37

When is a white FLARE displayed?

Answer 37

on a dual AP ILS approach only after LOC and G/S capture and below 1500 RA.

Question 38

What is LNAV capture criteria?

Answer 38

on any heading and w/in 3 NM of active route segment if outside 3 NM of active route segment: airplane must be on intercept course of 90° or less airplane must intercept the route segment before the active waypoint.

Question 39

A/T engages automatically when these AFDS modes are engaged:

Answer 39

``` LVL CHG ALT ACQ V/S VNAV ALT HOLD G/S capture TO/GA ```

Question 40

T/F:The A/T system can operate with EECs ON or ALTN

Answer 40

True. recommended either both EECs in ON mode or both in ALTN.

Question 41

Auto throttle disengagement happens how?

Answer 41

Moving A/T ARM switch OFF Pushing either A/T disengage switch An A/T fault detected 2 seconds have elapsed since landing touchdown.