Autoflight

Question 1

Pushing the altitude hold switch (ALT HLD) command pitch to hold
A corrected barometric altitude to the nearest 1000 feet at which the switch was pressed
B uncorrected barometric altitude at which the switch was pressed
C uncorrected radio altitude to the nearest 1000 feet at which the switch was pressed

Answer 1

B uncorrected barometric altitude at which the switch was pressed

Question 2

While the auto pilot is engaged, the use of Elec trim is
A prohibited
B allowed above Flight level 250
C allowed below flight level 250

Answer 2

A prohibited

Question 3

Pushing the LVL CHG button in a climb commands the auto throttles to hold
A idle thrust
B N1 limit thrust
C maximum thrust

Answer 3

B N1 limit thrust

Question 4

When you are climbing or descending with VNAV engaged, pushing the ALT INTV button will cause the next altitude restriction will be
A increased by 1000 feet
B change to correspond with altitude in the MCP altitude window
C eliminated

Answer 4

C eliminated

Question 5

Pushing the APP button switches arms, the AFDS for
A LNAV and VNAV capture only if a RNAV approach is selected in the FMC
B Any LNAV or VNAV capture
C localizer, or glideslope capture

Answer 5

C localizer, or glideslope capture

Question 6

What does FMC SPD indicate in the auto throttle mode FMA
A the auto throttle maintains thrust at the selected N1 limit displayed on the thrust mode display
B the auto throttle maintains speed set in the MCP IAS/MACH display
C the auto throttle maintains speed commanded by the FMC

Answer 6

C the auto throttle maintains speed commanded by the FMC

the autothrottle is limited to the N1 value shown on the mode display

Question 7

What does SINGLE CH indicate in the autopilot status display?
A for a single A/P ILS approach indicates the auto land system has completed all required test
B for a single A/P ILS approach in annunciates after localizer capture
C for a single A/P ILS approach annunciates below 2500 feet

Answer 7

B for a single A/P ILS approach in annunciates after localizer captured

Question 8

What does THR HLD indicate on the AFDS flight mode annunciations auto throttle mode?
A the auto throttle maintains the thrust at the selected N1 limit display on the thrust mode display
B no auto throttle mode engaged. The thrust lever auto throttle servers are inhibited. The pilot can set thrust manually
C the thrust lever auto throttle servers are inhibited; the pilot can set the thrust levers manually

Answer 8

C the thrust lever auto throttle servers are inhibited; the pilot can set the thrust lever manually

Question 9

To engage TO/GA mode for takeoff ________. You must press either TO/GA switch and.
A at least one FD switch must be ON
B both FD switches must be ON
C both FD switches must be OFF

Answer 9

B both FD switches must be ON

Question 10

What mode allows both A/Ps to be engaged at the same time (auto-land)
A APP
B VOR/LOC
C LNAV

Answer 10

A APP

Question 11

What does GA on the AFDS flight mode annunciations auto throttle mode indicate
A the auto throttle maintains thrust at reduced go round setting
B the throttle maintains thrust at the selected N1 limit displayed on the thrust mode display
C the auto throttle maintains speed, commanded by the FMC. The auto throttle is limited to the N1 value shown on the thrust mode display.

Answer 11

A the auto throttle maintains thrust at reduced go round setting

Question 12

The AFDS flight mode annunciation in the pitch mode VNAV SPD commands_______
A pitch to MCP selected altitude, or uncorrected barometric altitude
B AFDS to maintain altitude or decent path with pitch commands
C AFDS to maintain the FMC speed displayed in the airspeed indicator and or the CDU CLIMB or DESCENT pages

Answer 12

A the auto throttle maintains thrust at reduced go round setting

Question 13

Windchill scratching will occur if the windshield wipers are operated on______ windshield
A wet
B icy
C dry

Answer 13

C Dry

Question 14

What does arm on the AFDS flight mode annunciations auto throttle mode indicate
A no throttle mode, engaged the thrust lever auto throttle servers are inhibited. The pilot can set thrust manually.
B the thrust, the lever auto throttle servers are inhibited. The pilot can set the thrust levers manually.
C the auto throttle maintains thrust at the selected N1 limit display on the thrust mode display

Answer 14

A no throttle mode, engaged the thrust lever auto throttle servers are inhibited. The pilot can set thrust manually.

Question 15

On the mode, control panel, pushing the LNAV switch command, the AFDS role to intercept and track the active
A FMC route
B VOR radial
C LOC

Answer 15

A FMC route

Question 16

In a VNAV PTH decent the auto throttle hold______ and the AFDS_______
A idol holds IAS/MACH window
B idol, but can command FMC SPD mode if ground speed becomes too low to maintain FMC vertical path tracks FMC descent path
C idle holds FMC target speed

Answer 16

B idol, but can command FMC SPD mode if ground speed becomes too low to maintain FMC vertical path tracks FMC descent path

Question 17

What following indications regards ADS status annunciations are displayed in the a/P status display located above the attitude indicator
A CMD, FD, 1 CH
B CWS P, CWS R
C all answers are correct

Answer 17

C all answers are correct

Question 18

While in altitude hold, if the altitude selector on the mode, control panel is rotated the____[mode is armed
A VNAV
B V/S
C LVL CHG

Answer 18

B V/S

Question 19

All auto pilot flight Director systems ADS modes can be disengaged either by selecting another command mode or
A disengaging the a/P and turning the F/Ds off
B turning the F/Ds off
C by disengaging the A/P

Answer 19

A disengaging the a/P and turning the F/Ds off

Question 20

Auto land - Maximum tailwind for the B737 900 with flaps 30 with filled elevation of 4001–6000 feet_________
A 5 knots
B 10 knots
C 0 knots

Answer 20

A 5 knots

Question 21

What does CWS R and the auto pilot status display of the AFDS indicate?
A Pitch mode engaged and CWS
B roll mode, engaged in CWS
C the auto pilot is inoperative

Answer 21

B roll mode, engaged in CWS

Question 22

Auto land - maximum tailwind for the B7 37–900 with flaps 30 with Phil elevation 6001 feet and above is_______
A 10 knots
B 5 knots
C 0 knots

Answer 22

C 0 knots

Question 23

By engaging VNAV, the FMC command, the AFDS pitch and_________ to fly vertical profile selected on the________
A auto throttle; FMC CDUs
B LNAV; G/S
C auto throttle; G/S

Answer 23

A auto throttle; FMC CDUs

Question 24

What does RETARD on the AFDS Flight mode annunciations auto throttle mode indicate
A the auto throttle maintains speed, commanded by the FMC. The auto throttle is limited to N1 value shown on the thrust display.
B the auto throttle maintains thrust at the selected N1 limit display on the thrust mode display
C displayed while auto throttle move through labors to the aft stop RETARD mode is followed by a ARM mode

Answer 24

C displayed while auto throttle move through labors to the aft stop RETARD mode is followed by a ARM mode

Question 25

The vertical speed VRTSPEED display window_______ when the S is________ A blank; active B displays; not active C blanks; not active

Answer 25

C blanks; not active

Question 26

The bank angle selector sets the max bank angle for the ADS operation_______ modes A LNAV B HDG SEL or VOR C all answers are correct

Answer 26

B HDG SEL or VOR

Question 27

The AFDS flight mode, annunciation, in the pitch mode, ALT ACQ commands A a transition maneuver entered automatically from a V/S, LV CHG, or VNA climb or descent to the selected MCP altitude B the ADS to maintain the IAS/MACH window airspeed or MACH C pitch to MCP selected altitude or uncorrected barometric altitude

Answer 27

A a transition maneuver entered automatically from a V/S, LV CHG, or VNA climb or descent to the selected MCP altitude

Question 28

The AFDS flight mode, annunciation, in the pitch mode, VNAV PTH commands A the AFDS to maintain FMC altitude or decent path with pitch commands B the AFDS to maintain FMC speed displayed on the airspeed indicator/or CDUCLIM or DESCENT pages C pitch to MCP selected altitude, or uncorrected barometric altitude

Answer 28

A the AFDS to maintain FMC altitude or decent path with pitch commands

Question 29

The A/P automatically disengages when any of the following occurs A activating either pilot control, trim or loss of respective hydraulic system pressure B pushing either auto pilot disengage switch or pushing either takeoff/go-around TOGA to switch with a single auto pilot engaged in CWS or CMD below 2000 feet RA C all answers are correct

Answer 29

C all answers are correct

Question 30

What does CMD in the auto pilot status display of the AFDS indicate? A one or both auto parts are engaged B one or both auto pilots are disengaged C the flight Director is on and the auto pilot is either off or engaged in CWS

Answer 30

A one or both auto parts are engaged

Question 31

The AFDS flight mode, annunciation, in the pitch mode, MCP SPD commands_______ A pitch to MCP selected altitude, or uncorrected barometric altitude at which ALT HOLD switch was pushed B a transition maneuver entered automatically from a V/S, LV CHG, or VNA climb or descent to the selected MCP altitude C the AFDS to maintain the IAS/MACH window airspeed or MACH

Answer 31

C the AFDS to maintain the IAS/MACH window airspeed or MACH

Question 32

What does MCP SPD on the AFDS flight mode annunciations auto throttle mode indicate A the auto throttle maintains thrust at the selected N1 limit displayed on the thrust mode display B the auto throttle maintains speed set in the MCP IAS/MACH display. The autothrottle is limited to the N1 value shown on the thrust mode display C the auto throttle maintains speed commanded by the FMC. The autothrottle is limited to the N1 value shown on the thrust mode display

Answer 32

B the auto throttle maintains speed set in the MCP IAS/MACH display. The autothrottle is limited to the N1 value shown on the thrust mode display

Question 33

The F/Ds can be operated_________ A only with the A/P and A/T B with or without the A/P and A/T C only with A/T

Answer 33

B with or without the A/P and A/T

Question 34

How is the master FCC indicated? A by the illumination of the respective master MA F/D indicator light B by the illumination of the respective master caution indicator light C by the illumination of the CMD on respective FMA

Answer 34

A by the illumination of the respective master MA F/D indicator light

Question 35

To engage TO/GA for go round, press either TO/GA switch when A not in takeoff mode and either F/D switch on or off B in flight below 2000 feet altitude C all answers are correct

Answer 35

C all answers are correct

Question 36

Which steering command allows both A/Ps to be engaged at the same time A both Flight directors on B VNAV and VOR/LOC C the approach mode

Answer 36

C the approach mode

Question 37

Auto land maximum crosswind is A 20 knots B 10 knots C 15 knots

Answer 37

B 10 knots

Question 38

Auto land maximum crosswind is A 20 knots B 10 knots C 15 knots

Question 39

Pushing the level change, LVLCHG switch in a decent command, the auto throttle to hold______ thrust and the ADS to hold selected airspeed A limit B 1000 feet per minute C idle

Answer 39

C idle

Question 40

What does FD in the auto pilot status display of the AFDS indicate A the flight Director is on and the auto pilot is either off or engaged in CWS B both directors are disengaged C all answers are correct

Answer 40

A the flight Director is on and the auto pilot is either off or engaged in CWS

Question 41

Autoland maximum headwind is A 15 knots B 20 knots C 25 knots

Answer 41

C 25 knots

Question 42

What does N1 on the AFDS flight mode annunciation auto throttle mode indicate A the throttle maintains thrust at the selected N1 limit display on the thrust mode, display, including full, go around N1 setting B the auto throttle maintains speed, commanded by the FMC the auto throttle is limited to N1 value shown on the thrust mode dis C the auto throttle maintains thrust at a reduced go-round setting or full go around N1 limit

Answer 42

A the throttle maintains thrust at the selected N1 limit display on the thrust mode, display, including full, go around N1 setting

Question 43

The auto pilot flight Director system AFDS is a dual system consisting of _______ individual flight control, computers, FCC and a single mode control panel A three B two C one

Answer 43

B two

Question 44

What does SINGLE CH and the auto pilot status display of the AFS indicate? A For a single A/PILS approach, indicates that the auto land system has completed all required test and will function properly B for a single/ILS approach, annunciates after localizer capture and remains on for the entire approach C all answers are correct

Answer 44

B for a single/ILS approach, annunciates after localizer capture and remains on for the entire approach

Question 45

Initially, pushing the heading select HD GSEL switch commands a turn and the shortest direction toward the heading bug True False

Answer 45

True

Question 46

The AFDS Flight Mode Annunciation, in the Pitch Mode. G/S (engaged) commands ______________ A the AFDS to follow the ILS glideslope B the AFDS to maintain the IAS/MACH window airspeed or Mach C All answers are correct

Answer 46

A the AFDS to follow the ILS glideslope

Question 47

Pushing the speed intervention, SPD INT switch on the mode control panel when VA is engaged A reveals the IAS/MACH display activates FMC speed intervention displays the FMC target speed and allows the IAS/MACH selector to be used to set the desired speed B is prohibited C blanks the IAS/MACH display activates the VNAPHTH and disengages the A/T

Answer 47

A reveals the IAS/MACH display activates FMC speed intervention displays the FMC target speed and allows the IAS/MACH selector to be used to set the desired speed