Section 2: Autoflight Learning Objectives Flashcards

1
Q

AUTO_005 V2 22_30.20

Recall what modes are engaged when FDs are initially turned on in flight (assuming the AP is OFF).

FDs engage in the _____ and ____ modes.

A

AUTO_005 V2 22_30.20

Recall what modes are engaged when FDs are initially turned on in flight (assuming the AP is OFF).

FDs engage in the HDG and V/S modes.

V2 22_30.20

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2
Q

AUTO_015 FCTM 1.10

Recall the scenario in which it is desirable or acceptable to have only one FD engaged.

A

AUTO_015 FCTM 1.10

Recall the scenario in which it is desirable or acceptable to have only one FD engaged.

There is no scenario in which it is desirable or acceptable to have only one FD engaged.

FCTM 1.10

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3
Q

AUTO_020 FCTM 1.10

Recall what should be done with the FDs if they are not to be followed.

A

AUTO_020 FCTM 1.10

Recall what should be done with the FDs if they are not to be followed.

If the flight director commands are not to be followed, both flight directors should be turned off.

FCTM 1.10

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4
Q

AUTO_025 FCTM 1.10

Recall the autothrust mode when both FDs and the AP are selected off.

A

AUTO_025 FCTM 1.10

Recall the autothrust mode when both FDs and the AP are selected off.

Speed mode (green SPEED or MACH indicated in column 1 of the FMA).

FCTM 1.10

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5
Q

AUTO_030 FCTM 1.10

Recall the recommended method for disconnecting the autothrust.

A

AUTO_030 FCTM 1.10

Recall the recommended method for disconnecting the autothrust.

Match the thrust levers to the actual thrust value (use the TLA “donuts”) then press either red instinctive disconnect push button on the thrust levers.

FCTM 1.10

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6
Q

AUTO_035. V2 22_40.10

Recall what is displayed in FMA column 3 when the FCU HDG/TRK knob is pulled during flight.

A

AUTO_035. V2 22_40.10

Recall what is displayed in FMA column 3 when the FCU HDG/TRK knob is pulled during flight.

HDG in green (TRK in green if TRK/FPA mode is selected on FCU).

V2 22_40.10

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7
Q

AUTO_040 V2 22_40.10

Recall what is displayed in FMA column 3 when the FCU HDG/TRK knob is pushed during flight.

If the aircraft is on the FMS flight plan course, column 3 will indicate _____ in green.

If the aircraft is on a heading that will intercept the flight plan course, column 3 will indicate ___ (color) with ____ _____ (color).

A

AUTO_040 V2 22_40.10

Recall what is displayed in FMA column 3 when the FCU HDG/TRK knob is pushed during flight.

If the aircraft is on the FMS flight plan course, column 3 will indicate NAV in green.

If the aircraft is on a heading that will intercept the flight plan course, column 3 will indicate HDG (green) with NAV armed (blue).

V2 22_40.10

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8
Q

AUTO_045 V2 22_30.40

Recall the difference between a blue and magenta target airspeed symbol (triangle) on the airspeed tape.

Blue triangle: ______ ________

Magenta triangle: ______ _______

A

AUTO_045 V2 22_30.40

Recall the difference between a blue and magenta target airspeed symbol (triangle) on the airspeed tape.

Blue triangle: Selected Speed

Magenta triangle: Managed Speed

V2 22_30.40

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9
Q

AUTO_050 V2 22_30.20

Recall the normal FMA indications in column 5 after the preflight is complete.

______ if both FDs are ON and both ______ are functioning.

A

AUTO_050 V2 22_30.20

Recall the normal FMA indications in column 5 after the preflight is complete.

1FD2 if both FDs are ON and both FMGCs are functioning.

V2 22_30.20

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10
Q

AUTO_055 V2 22_10.40

Recall the basic color conventions used in the MCDU regarding pilot data entry.

_____: Data that is modifiable by the pilot

_____: Data that is not modifiable by the pilot

_____: Data that must be entered by the pilot

A

AUTO_055 V2 22_10.40

Recall the basic color conventions used in the MCDU regarding pilot data entry.

Blue: Data that is modifiable by the pilot

Green: Data that is not modifiable by the pilot

Amber: Data that must be entered by the pilot

V2 22_10.40

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11
Q

AUTO_060 VOL 1 NP.3.4

Recall the value to be manually entered in the FINAL field on the INIT page B.

The _______ fuel value from the FLIGHT PLAN ______ block of the flight paperwork.

A

AUTO_060 VOL 1 NP.3.4

Recall the value to be manually entered in the FINAL field on the INIT page B.

The RESERVE fuel value from the FLIGHT PLAN FUEL block of the flight paperwork.

VOL 1 NP.3.4

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12
Q

AUTO_065 VOL 1 NP.3.4

Recall the value to be manually entered in the ALTN field on the INIT page B.

The _______ fuel value from the FLIGHT PLAN _____ ______ of the flight paperwork.

If ____ ______ are specified, the value from the most ______ alternate.

A

AUTO_065 VOL 1 NP.3.4

Recall the value to be manually entered in the ALTN field on the INIT page B.

The ALTN fuel value from the FLIGHT PLAN FUEL block of the flight paperwork.

If two alternates are specified, the value from the most distant alternate.

VOL 1 NP.3.4

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13
Q

AUTO_070 FCTM 3.1

Recall whether CLB or ALT should be armed in column 2 of the FMA before takeoff.

A

AUTO_070 FCTM 3.1

Recall whether CLB or ALT should be armed in column 2 of the FMA before takeoff.

CLB

FCTM 3.1

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14
Q

AUTO_075 V2 22_30.100

Recall what is displayed in column 3 of the FMA before takeoff.

With no heading preselected, ___ is armed (color). With a heading preselected, column 3 is ______.

A

AUTO_075 V2 22_30.100

Recall what is displayed in column 3 of the FMA before takeoff.

With no heading preselected, NAV is armed (blue). With a heading preselected, column 3 is blank.

V2 22_30.100

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15
Q

AUTO_090 V2 31.40

Recall which V-speeds are visible on the PFD during taxi out.

V__ (_____) and

V___ (______).

A

AUTO_090 V2 31.40

Recall which V-speeds are visible on the PFD during taxi out.

V1 (blue) and

V2 (magenta).

V2 31.40

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16
Q

AUTO_100 V2 22_30.90

Recall the FMA column 1 indications during takeoff when the thrust levers are placed in the CL, FLX/MCT, or TOGA detents:

CL detent: Column 1 is _____ and an ____ ___ _____ NOT SET ECAM message appears

FLX/MCT detent:

o MAN FLX ___\_ assuming a ____ ____ is entered on the ____ ____ ____ page.
o With no ___ _____ entered, Column 1 is _____ and an ____ ___ _____ NOT SET ECAM message appears.

• TOGA detent: _____ ______.

A

AUTO_100 V2 22_30.90

Recall the FMA column 1 indications during takeoff when the thrust levers are placed in the CL, FLX/MCT, or TOGA detents:

CL detent: Column 1 is blank and an ENG THR LEVERS NOT SET ECAM message appears

FLX/MCT detent:

o MAN FLX (Temp)assuming a FLEX TEMP is entered on the PERF TAKE OFF page.
o With no FLEX TEMP entered, Column 1 is blank and an ENG THR LEVERS NOT SET ECAM message appears.

• TOGA detent: MAN TOGA.

V2 22_30.90

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17
Q

AUTO_105 V2 22_30.100 FCTM 3.1

Takeoff & Initial Climb

Recall the FMA column 5 indication when the thrust levers are placed in FLX/MCT or TOGA.

_/___ (_____)

A

AUTO_105 V2 22_30.100 FCTM 3.1

Takeoff & Initial Climb

Recall the FMA column 5 indication when the thrust levers are placed in FLX/MCT or TOGA.

A/THR (blue)

V2 22_30.100 FCTM 3.1

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18
Q

AUTO_110 V2 22_20.20

Recall the actions required to tune the localizer signal for takeoff.

A

AUTO_110 V2 22_20.20

Recall the actions required to tune the localizer signal for takeoff.

None. Tuning is automatic when the takeoff runway has an associated ILS.

V2 22_20.20

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19
Q

AUTO_115 V2 22_30.80

Recall the indications in FMA column 3 after FLX/MCT or TOGA is selected during takeoff.

If there is no localizer signal, column 3 is ______.

If there is a localizer signal, ____ (color) appears.

A

AUTO_115 V2 22_30.80

Recall the indications in FMA column 3 after FLX/MCT or TOGA is selected during takeoff.

If there is no localizer signal, column 3 is blank.

If there is a localizer signal, RWY (green) appears.

V2 22_30.80

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20
Q

AUTO_120 V2 22_30.10

Recall the altitude at which the NAV mode becomes active after takeoff without a pre- selected heading.

A

AUTO_120 V2 22_30.10

Recall the altitude at which the NAV mode becomes active after takeoff without a pre- selected heading.

30’

V2 22_30.10

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21
Q

AUTO_125 V2 22_30.10 V2 22_30.60

Recall the initial lateral mode the aircraft will fly after a takeoff with a preselected heading and the action necessary to provide FD heading guidance at 400’.

___ _____ (the aircraft track at the time of engagement - 30 ft).

Pull the ___/_____ knob.

A

AUTO_125 V2 22_30.10 V2 22_30.60

Recall the initial lateral mode the aircraft will fly after a takeoff with a preselected heading and the action necessary to provide FD heading guidance at 400’.

RWY TRK (the aircraft track at the time of engagement - 30 ft).

Pull the HDG/TRK knob.

V2 22_30.10 V2 22_30.60

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22
Q

AUTO_135 FCTM 3.1 V2 22_30.80

Recall the speed the aircraft will fly in SRS mode during takeoff, assuming both engines are operating.

V_+__

A

AUTO_135 FCTM 3.1 V2 22_30.80

Recall the speed the aircraft will fly in SRS mode during takeoff, assuming both engines are operating.

V2+10

FCTM 3.1 V2 22_30.80

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23
Q

AUTO_145 V1 NP.3.4

Recall how the thrust reduction (THR RED) and acceleration (ACC) altitudes are inserted into the PERF TAKE OFF page.

They are uplinked via the _____ process.

______ entry may be required to comply with Company Page (10-7) information.

A

AUTO_145 V1 NP.3.4

Recall how the thrust reduction (THR RED) and acceleration (ACC) altitudes are inserted into the PERF TAKE OFF page.

They are uplinked via the TDU process.

Manual entry may be required to comply with Company Page (10-7) information.

V1 NP.3.4

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24
Q

AUTO_150 V2 22_30.80

Takeoff & Initial Climb:

Recall when the SRS (Speed Reference System) vertical mode automatically disengages and what vertical mode replaces SRS.

SRS disengages:

  1. SRS automatically disengages at _____ _____ and reverts to ____ (or __ ___ if in HDG).
  2. If the flight crew engages another ______ mode.
A

AUTO_150 V2 22_30.80

Takeoff & Initial Climb:

Recall when the SRS (Speed Reference System) vertical mode automatically disengages and what vertical mode replaces SRS.

SRS disengages:

  1. SRS automatically disengages at acceleration altitude and reverts to CLB (or OP CLB if in HDG).
  2. If the flight crew engages another vertical mode.
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25
Q

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

When thrust levers placed in the ______ detent:

A

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

When thrust levers placed in the TOGA detent:

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26
Q

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

At 30’ RA

A

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

At 30’ RA

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27
Q

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

At Thrust Reduction Altitude and Acceleration Altitude (1000’):

A

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

At Thrust Reduction Altitude and Acceleration Altitude (1000’):

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28
Q

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

After Thrust Reduction (T/Ls placed into CL detent):

A

AUTO_155 FCTM 3.10

Recall the FMA columns 1, 2, 3, and 5 indications during takeoff and initial climb assuming an NADP2 departure, TOGA thrust, and NAV armed.

After Thrust Reduction (T/Ls placed into CL detent):

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29
Q

AUTO_ 165 FCTM 4.1

(Climb)

Recall the normal target airspeed after passing the acceleration altitude and until passing 10,000’ MSL (assuming no speed constraints in the F-PLN).

The FMS targets the _____ ______ ____ stored in the navigation database for the departure airport (normally _____ knots at or below 10,000 feet MSL).

A

AUTO_ 165 FCTM 4.1

(Climb)

Recall the normal target airspeed after passing the acceleration altitude and until passing 10,000’ MSL (assuming no speed constraints in the F-PLN).

The FMS targets the transition speed limit stored in the navigation database for the departure airport (normally 250 knots at or below 10,000 feet MSL).

FCTM 4.1

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30
Q

AUTO_170 FCTM 4.1

Recall how to enter a pre-selected climb speed.

A pre-selected speed may be entered on the

____ _____ page prior to entering the ____ phase.

It has the same effect as selecting a speed on the ____ after passing the acceleration altitude.

A

AUTO_170 FCTM 4.1

Recall how to enter a pre-selected climb speed.

A pre-selected speed may be entered on the PERF CLB page prior to entering the climb phase.

It has the same effect as selecting a speed on the FCU after passing the acceleration altitude.

FCTM 4.1

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31
Q

AUTO_175 FCTM 4.1

Recall the suggested method of increasing the rate of climb during an Open Climb or Managed Climb.

Selecting a _______ speed on the FCU.

A

AUTO_175 FCTM 4.1

Recall the suggested method of increasing the rate of climb during an Open Climb or Managed Climb.

Selecting a slower speed on the FCU.

FCTM 4.1

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32
Q

AUTO_180 V2 31.40

Recall the appropriate action if ATC temporarily assigns a specific speed during the climb and the action required when ATC states “resume normal speed” after a temporary speed assignment.

  1. Select the assigned speed in the SPD/MACH window and then ____ the SPD/MACH knob.

OR

  1. ______ the SPD/MACH knob to resume the normal ECON climb speed.
A

AUTO_180 V2 31.40

Recall the appropriate action if ATC temporarily assigns a specific speed during the climb and the action required when ATC states “resume normal speed” after a temporary speed assignment.

  1. Select the assigned speed in the SPD/MACH window and then pull the SPD/MACH knob.

OR

  1. Push the SPD/MACH knob to resume the normal ECON climb speed.

V2 31.40

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33
Q

AUTO_185 FCTM 4.1

Recall what speed to use to achieve the maximum angle of climb.

Green dot equates to the _____ ____ of _____.

Either select ____ ____ in the FCU OR

push the ______ pb.

A

AUTO_185 FCTM 4.1

Recall what speed to use to achieve the maximum angle of climb.

Green dot equates to the maximum angle of climb.

Either select green dot in the FCU or

push the EXPED pb.

FCTM 4.1

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34
Q

AUTO_190 V2 22_30.100 FCTM 4.1

Recall the FMA column 1 and 2 indications when the EXPED pb is pushed during a climb.

Columns 1 and 2 will indicate ____ ____ and

___ ____ , respectively.

A

AUTO_190 V2 22_30.100 FCTM 4.1

Recall the FMA column 1 and 2 indications when the EXPED pb is pushed during a climb.

Columns 1 and 2 will indicate THR CLB and EXP CLB, respectively.

V2 22_30.100 FCTM 4.1

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35
Q

AUTO_195 FCTM 4.1

Recall the maximum recommended altitude for the EXP CLB mode.

A

AUTO_195 FCTM 4.1

Recall the maximum recommended altitude for the EXP CLB mode.

FL250

FCTM 4.1

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36
Q

AUTO_200 FCTM 4.1

Recall the recommended climb mode, and the FMA column 2 indication of that mode, when a departure procedure includes altitude constraints.

______ Climb, indicated by ____ in (color).

A

AUTO_200 FCTM 4.1

Recall the recommended climb mode, and the FMA column 2 indication of that mode, when a departure procedure includes altitude constraints.

Managed Climb, indicated by CLB in green.

FCTM 4.1

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37
Q

AUTO_205 FCTM 4.1

Recall which vertical mode should be used, and what altitude should be set in the FCU, when cleared to climb-via a SID with altitude constraints:

_____ _______ should be used, and the _______ cleared altitude should be set in the FCU.

A

AUTO_205 FCTM 4.1

Recall which vertical mode should be used, and what altitude should be set in the FCU, when cleared to climb-via a SID with altitude constraints.

Managed Climb should be used, and the highest cleared altitude should be set in the FCU.

FCTM 4.1

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38
Q

AUTO_210 FCTM 4.1

Recall what lateral mode must be active for a Managed Climb to be engaged, and the resulting climb mode if assigned a heading while performing a Managed Climb on a SID:

______ ____ (green ____ in FMA column _).

The FMS reverts to __ ___ when the lateral mode is changed to HDG (e.g., ATC assigns a heading for spacing).

A

AUTO_210 FCTM 4.1

Recall what lateral mode must be active for a Managed Climb to be engaged, and the resulting climb mode if assigned a heading while performing a Managed Climb on a SID.

Managed Nav (green NAV in FMA column 3).

The FMS reverts to OP CLB when the lateral mode is changed to HDG (e.g., ATC assigns a heading for spacing).

FCTM 4.1

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39
Q

AUTO_215 FCTM 4.1

Recall the thrust setting used by the autothrust system and the column 1 indication in the FMA when a Managed Climb is engaged:

_______; ___ ____

A

AUTO_215 FCTM 4.1

Recall the thrust setting used by the autothrust system and the column 1 indication in the FMA when a Managed Climb is engaged:

Climb thrust; THR CLB

FCTM 4.1

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40
Q

AUTO_220 V2 22_20.30

Recall how to enter an AT, AT OR BELOW, or AT OR ABOVE altitude climb constraint at a waypoint directly on the F-PLN page.

AT:

AT OR BELOW:

AT OR ABOVE:

A

AUTO_220 V2 22_20.30

Recall how to enter an AT, AT OR BELOW, or AT OR ABOVE altitude climb constraint at a waypoint directly on the F-PLN page.

AT: Enter /____ (altitude or flight level) into the scratchpad and then the appropriate R LSK. /250

AT OR BELOW: Enter /-___ (altitude or flight level) into the scratchpad and then the appropriate R LSK.

/-250

AT OR ABOVE: Enter /+____ (altitude or flight level) into the scratchpad and then the appropriate R LSK.

/+250

V2 22_20.30

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41
Q

AUTO_225 V2 22_20.30

Recall how to enter a speed constraint at a waypoint directly on the F-PLN page:

A

AUTO_225 V2 22_20.30

Recall how to enter a speed constraint at a waypoint directly on the F-PLN page.

Enter the speed (ex. 180) into the scratchpad and insert at the appropriate R LSK.

V2 22_20.30

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42
Q

AUTO_235 V2 22_20.40

Recall the indications if the FMS predicts that an AT or AT OR ABOVE climb constraint can and cannot be met during a Managed Climb:

Can be met: ________ circle around the waypoint symbol on the ___ and an

______ asterisk next to the altitude constraint in the ______.

Cannot be met: ______ circle around the waypoint symbol on the ___ and an

_____ asterisk next to the altitude constraint in the ______.

A

AUTO_235 V2 22_20.40

Recall the indications if the FMS predicts that an AT or AT OR ABOVE climb constraint can and cannot be met during a Managed Climb.

Can be met: Magenta circle around the waypoint symbol on the ND and anmagenta asterisk next to the altitude constraint in the MCDU.

Cannot be met: Amber circle around the waypoint symbol on the ND and anamber asterisk next to the altitude constraint in the MCDU.

V2 22_20.40

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43
Q

AUTO_240 FCTM 4.1

Recall the suggested pilot action if the FMS predicts that an AT or AT OR ABOVE constraint will not be met during a Managed Climb.

Increase the rate of climb by selecting a _______ speed.

A

AUTO_240 FCTM 4.1

Recall the suggested pilot action if the FMS predicts that an AT or AT OR ABOVE constraint will not be met during a Managed Climb.

Increase the rate of climb by selecting a slower speed.

FCTM 4.1

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44
Q

AUTO_245 FCTM 4.1

Recall the indications in column 2 of the FMA if the aircraft must temporarily level-off in order to satisfy an AT or AT OR BELOW constraint during a Managed Climb:

A

AUTO_245 FCTM 4.1

Recall the indications in column 2 of the FMA if the aircraft must temporarily level-off in order to satisfy an AT or AT OR BELOW constraint during a Managed Climb.

Magenta ALT

FCTM 4.1

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45
Q

AUTO_260

Recall if altitude constraints are honored in an OP CLB.

They are _______, as indicated by a ______ circle around the waypoint.

A

AUTO_260 V2 22_30.100

Recall if altitude constraints are honored in an OP CLB.

They are ignored, as indicated by a white circle around the waypoint.

V2 22_30.100

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46
Q

AUTO_265 V2 22_10.40

Recall what occurs if the V/S or FPA knob is pushed during a climb.

The autoflight system commands an ______ _____-____

A

AUTO_265 V2 22_10.40

Recall what occurs if the V/S or FPA knob is pushed during a climb.

The autoflight system commands an immediate level-off.

V2 22_10.40

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47
Q

AUTO_275 FCTM 4.1

Recall what occurs if an excessive V/S is selected during a climb.

A

AUTO_275 FCTM 4.1

Recall what occurs if an excessive V/S is selected during a climb.

Airspeed decreases below the target airspeed in an attempt to achieve the selected V/S.

FCTM 4.1

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48
Q

AUTO_280 V2 22_3

Recall the effect of changing the FCU altitude while ALT* is active in FMA column 2.

The vertical mode reverts to the current ______ _______.

A

AUTO_280 V2 22_3

Recall the effect of changing the FCU altitude while ALT* is active in FMA column 2.

The vertical mode reverts to the current vertical speed.

V2 22_3

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49
Q

AUTO_285 V2 22_20.50

(Cruise)

Recall the significance of the three altitudes on the FMS PROG page.

CRZ (blue):CRZ Flight level inserted on ____ Pge _ or directly on _____ page. This field shows _____ when the descent or approach phase is active.

OPT: Optimum flight level based on current _____, ____ index, ______ and _____.

REC MAX: Recommended Max Altitude based on current _____ and _____, assuming anti-ice is off, and provides a 0._ g buffet margin.

A

AUTO_285 V2 22_20.50

(Cruise)

Recall the significance of the three altitudes on the FMS PROG page.

CRZ (blue): CRZ Flight level inserted on INIT Page A or directly on PROG page. This field shows dashes when the descent or approach phase is active.

OPT: Optimum flight level based on current weight, cost index, temperature and wind.

REC MAX: Recommended Max Altitude based on current weight and temperature, assuming anti-ice is off, and provides a 0.3g buffet margin.

V2 22_20.50

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50
Q

AUTO_290 V22_20.30

(Cruise)

Recall the effect of entering a down path waypoint into the F-PLN using the scratchpad and LSKs.

This automatically _______ the flight plan, ______ intermediate waypoints that are now __ _____ part of the route.

A

AUTO_290 V22_20.30

(Cruise)

Recall the effect of entering a down path waypoint into the F-PLN using the scratchpad and LSKs.

This automatically sequences the flight plan, eliminating intermediate waypoints that are now no longer part of the route.

51
Q

AUTO_295 V2 22_20.30

Recall the effect of entering a NEW DEST after an upcoming waypoint.

Subsequent F-PLN waypoints are ______ and the new DEST airport appears immediately after the waypoint.

A

AUTO_295 V2 22_20.30

Recall the effect of entering a NEW DEST after an upcoming waypoint.

Subsequent F-PLN waypoints are deleted and the new DEST airport appears immediately after the waypoint.

V2 22_20.30

52
Q

AUTO_300 OE.2

(Cruise)

Recall what approach transitions (VIAs) are available when a STAR is inserted into the F- PLN.

Only those approach transitions (VIAs) that are ________ with the inserted STAR

A

AUTO_300 OE.2

(Cruise)

Recall what approach transitions (VIAs) are available when a STAR is inserted into the F- PLN.

Only those approach transitions (VIAs) that are compatible with the inserted STAR

OE.2

53
Q

AUTO_305 OE.2

Recall how to make additional approach transitions (VIAs) available after a STAR has been inserted into the F-PLN.

Insert _____ ______

A

AUTO_305 OE.2

Recall how to make additional approach transitions (VIAs) available after a STAR has been inserted into the F-PLN.

Insert NO STAR

OE.2

54
Q

AUTO_315 V2 22_30.70

Recall the difference between an Idle-Path and Geometric-Path descent profile.

An idle-path descent is a planned descent profile assuming ____ _____.

A geometric path descent profile assumes a ____ line descent from one waypoint to the next.

A

AUTO_315 V2 22_30.70

Recall the difference between an Idle-Path and Geometric-Path descent profile.

An idle-path descent is a planned descent profile assuming idle thrust.

A geometric path descent profile assumes a straight line descent from one waypoint to the next.

V2 22_30.70

55
Q

AUTO_325 FCTM 4.3

(Descent)

Recall what to do when a Mach-to-IAS transition speed is published on a STAR.

_______ enter the required speed using the MACH/IAS format into the PERF _____ page prior to _____.

A

AUTO_325 FCTM 4.3

(Descent)

Recall what to do when a Mach-to-IAS transition speed is published on a STAR.

Manually enter the required speed using the MACH/IAS format into the PERF DES page prior to TOD.

FCTM 4.3

56
Q

AUTO_330 FCTM 4.3

Recall which altitude constraints are not automatically inserted when a STAR is loaded in the F-PLN.

A

AUTO_330 FCTM 4.3

Recall which altitude constraints are not automatically inserted when a STAR is loaded in the F-PLN.

“Expect” constraints

FCTM 4.3

57
Q

AUTO_335 V2 22_20.30

Recall how to enter an AT, AT OR BELOW, or AT OR ABOVE altitude descent constraint at a waypoint directly on the F-PLN page.

AT:

AT OR BELOW:

AT OR ABOVE:

A

AUTO_335 V2 22_20.30

Recall how to enter an AT, AT OR BELOW, or AT OR ABOVE altitude descent constraint at a waypoint directly on the F-PLN page.

AT: Enter /___(altitude or flight level) into the scratchpad and then the appropriate R LSK. /230

AT OR BELOW: Enter /-___ (altitude or flight level) into the scratchpad and then the appropriate R LSK.

/-230

AT OR ABOVE: Enter /+___(altitude or flight level) into the scratchpad and then the appropriate R LSK.

/+230

V2 22_20.30

58
Q

AUTO_340 V2 22_20.30

Recall how to enter a descent SPEED constraint at a waypoint directly on the F-PLN page.

A

AUTO_340 V2 22_20.30

Recall how to enter a descent SPEED constraint at a waypoint directly on the F-PLN page.

• Enter (speed)/ into the scratchpad and then the appropriate R LSK.

V2 22_20.30

59
Q

AUTO_345 FCTM 4.3

Recall how the top-of-descent (TOD) is depicted on the ND.

The TOD is displayed on the ND track as a _____ _____ arrow

A

AUTO_345 FCTM 4.3

Recall how the top-of-descent (TOD) is depicted on the ND.

The TOD is displayed on the ND track as a white downward arrow.

FCTM 4.3

60
Q

AUTO_350 FCTM 4.3

Recall the warning should the top-of-descent (TOD) point be overflown (while in managed speed).

______ message displayed on the _____ and ______.

A

AUTO_350 FCTM 4.3

Recall the warning should the top-of-descent (TOD) point be overflown (while in managed speed).

DECELERATE message displayed on the MCDU and PFD.

FCTM 4.3

61
Q

AUTO_355 FCTM 4.3

Recall what the FCU altitude window should be set to when cleared to descend-via a STAR with altitude constraints.

If the DES mode is maintained as the active vertical mode, the _____ ______ ______ may be set in the FCU altitude window.

A

AUTO_355 FCTM 4.3

Recall what the FCU altitude window should be set to when cleared to descend-via a STAR with altitude constraints.

If the DES mode is maintained as the active vertical mode, the lowest altitude restriction may be set in the FCU altitude window.

FCTM 4.3

62
Q

AUTO_360 FCTM 4.3

Recall whether or not a descent is initiated automatically from cruise flight.

A

AUTO_360 FCTM 4.3

Recall whether or not a descent is initiated automatically from cruise flight.

An initial descent will not begin without pilot action (there is no “arming” the descent).

FCTM 4.3

63
Q

AUTO_365 FCTM 4.3

Recall the recommended descent mode, and the FMA column 2 indication of that mode, when an arrival procedure includes altitude constraints.

A

AUTO_365 FCTM 4.3

Recall the recommended descent mode, and the FMA column 2 indication of that mode, when an arrival procedure includes altitude constraints.

Managed Descent, indicated by DES in green.

FCTM 4.3

64
Q

AUTO_370 FCTM 4.3

Recall the expected descent behavior when a Managed Descent is initiated before the top-of-descent (TOD).

A

AUTO_370 FCTM 4.3

Recall the expected descent behavior when a Managed Descent is initiated before the top-of-descent (TOD).

If DES is engaged before the top of descent point, the FMS will command a gentle initial descent of 1,000 feet/min (in some cases 500 feet/min).

This descent rate will continue until intercepting the planned profile or reaching the altitude selected on the FCU.

FCTM 4.3

65
Q

AUTO_375 FCTM 4.3

Recall what lateral mode must be active for a Managed Descent.

A

AUTO_375 FCTM 4.3

Recall what lateral mode must be active for a Managed Descent.

NAV or LOC

FCTM 4.3

66
Q

AUTO_380 FCTM 4.3

Recall the column 2 FMA indication of a Managed Descent.

A

AUTO_380 FCTM 4.3

Recall the column 2 FMA indication of a Managed Descent.

DES in green

FCTM 4.3

67
Q

AUTO_385 FCTM 4.3

Recall the indication where the descent profile will be intercepted when initiating a Managed Descent early (i.e., before the Top-of-Descent).

The point where the descent profile will be intercepted is displayed on the ND as a ___ _______ _______.

A

AUTO_385 FCTM 4.3

Recall the indication where the descent profile will be intercepted when initiating a Managed Descent early (i.e., before the Top-of-Descent).

The point where the descent profile will be intercepted is displayed on the ND as a blue lightning bolt.

FCTM 4.3

68
Q

AUTO_390 FCTM 4.3

Recall the action required if ATC temporarily assigns a speed during the descent.

  1. Select the assigned speed in the _____/____ and ____ the _____/____ knob, or
  2. Enter the speed in the _____ DES page.
A

AUTO_390 FCTM 4.3

Recall the action required if ATC temporarily assigns a speed during the descent.

  1. Select the assigned speed in the SPD/MACH window and pull the SPD/MACH knob, or
  2. Enter the speed in the PERF DES page.

FCTM 4.3

69
Q

AUTO_395 FCTM

Recall the action required when ATC states “resume normal speed” after a temporary speed assignment.

If in selected speed, push the ___/____ knob.

If in Managed Speed, _____ the inserted speed on the PERF DES page.

A

AUTO_395 FCTM

Recall the action required when ATC states “resume normal speed” after a temporary speed assignment.

If in selected speed, push the SPD/MACH knob.

If in Managed Speed, clear the inserted speed on the PERF DES page.

FCTM

70
Q

AUTO_400 V2 22_20.40

Recall the indications if the FMS predicts that an AT or AT OR BELOW descent constraint cannot be met during a Managed Descent.

An ______ circle around the constrained waypoint.

Additionally an _____ asterisk next to the inserted constraint.

A

AUTO_400 V2 22_20.40

Recall the indications if the FMS predicts that an AT or AT OR BELOW descent constraint cannot be met during a Managed Descent.

An amber circle around the constrained waypoint.

Additionally an amber asterisk next to the inserted constraint.

V2 22_20.40

71
Q

AUTO_405 V2 22_20.40

Recall the indications if the FMS predicts that an AT or AT OR BELOW descent constraint will be met during a Managed Descent.

A _______ circle around the constrained waypoint. Additionally a ______ asterisk next to the inserted constraint.

A

AUTO_405 V2 22_20.40

Recall the indications if the FMS predicts that an AT or AT OR BELOW descent constraint will be met during a Managed Descent.

A magenta circle around the constrained waypoint. Additionally a magenta asterisk next to the inserted constraint.

V2 22_20.40

72
Q

AUTO_410 FCTM 4.3

Understand the effect of speedbrakes when descending on the VNAV path.

(speedbrakes _______ aid in increasing the descent rate while on the VNAV path).

A

AUTO_410 FCTM 4.3

Understand the effect of speedbrakes when descending on the VNAV path.

Application of speedbrakes while on the VNAV path will result in the aircraft remaining on the VNAV managed descent path

(speedbrakes do not aid in increasing the descent rate while on the VNAV path).

FCTM 4.3

73
Q

AUTO_415 FCTM 4.1

Recall the resulting descent mode if ATC assigns a heading while performing a Managed Descent on a STAR.

The vertical descent mode reverts to the current ____ when the lateral mode reverts to ____.

A

AUTO_415 FCTM 4.1

Recall the resulting descent mode if ATC assigns a heading while performing a Managed Descent on a STAR.

The vertical descent mode reverts to the current V/S when the lateral mode reverts to HDG.

FCTM 4.1

74
Q

AUTO_420 FCTM 4.3

Recall the strategy that can be used if cleared direct to a downline waypoint on a STAR and the pilot wishes to retain the descent profile as determined by the intermediate waypoint altitude constraints.

If intermediate waypoints are relevant, (e.g., for terrain awareness, etc.) then “___ ___ ” with ____ ____ may be an appropriate selection as constraints can be ______ into these waypoints if required.

A

AUTO_420 FCTM 4.3

Recall the strategy that can be used if cleared direct to a downline waypoint on a STAR and the pilot wishes to retain the descent profile as determined by the intermediate waypoint altitude constraints.

If intermediate waypoints are relevant, (e.g., for terrain awareness, etc.) then “DIR TO” with ABEAM PTS may be an appropriate selection as constraints can be re-entered into these waypoints if required.

FCTM 4.3

75
Q

AUTO_425 FCTM 4.1

Recall the indications in FMA column 2 if the aircraft must temporarily level-off in order to satisfy an AT or an AT OR ABOVE constraint during a Managed Descent.

A

AUTO_425 FCTM 4.1

Recall the indications in FMA column 2 if the aircraft must temporarily level-off in order to satisfy an AT or an AT OR ABOVE constraint during a Managed Descent.

Magenta ALT

FCTM 4.1

76
Q

AUTO_430 FCTM 4.3

Recall what occurs after the aircraft passes a waypoint where a temporary level-off was necessary during the descent to satisfy an altitude constraint (assuming the FCU altitude is set to a lower altitude).

After the target altitude constraint is passed, the _____ mode will engage and the aircraft will ______ the descent.

A

AUTO_430 FCTM 4.3

Recall what occurs after the aircraft passes a waypoint where a temporary level-off was necessary during the descent to satisfy an altitude constraint (assuming the FCU altitude is set to a lower altitude).

After the target altitude constraint is passed, the DES mode will engage and the aircraft will continue the descent.

FCTM 4.3

77
Q

AUTO_435 FCTM 4.3

Recall some ways to regenerate a new top-of-descent point of an idle path after leveling off at an intermediate altitude during the descent.

___ ___ any waypoint,

___ ____ addition, change, or deletion at the TO waypoint,

Change or reinsertion of ___/____ on the PERF DES page, or

___ ____ (__) change or reinsertion.

A

AUTO_435 FCTM 4.3

Recall some ways to regenerate a new top-of-descent point of an idle path after leveling off at an intermediate altitude during the descent.

DIR TO any waypoint,

ALT CSTR addition, change, or deletion at the TO waypoint,

Change or reinsertion of SPD/Mach on the PERF DES page, or

Cost Index (CI) change or reinsertion.

FCTM 4.3

78
Q

AUTO_440 FCTM 4.3

Recall what assumption is made by the blue lightning bolt (point where aircraft will intercept the path) if the aircraft has deviated above the descent profile.

_____ speed-brakes are used.

A

AUTO_440 FCTM 4.3

Recall what assumption is made by the blue lightning bolt (point where aircraft will intercept the path) if the aircraft has deviated above the descent profile.

Half speed-brakes are used.

FCTM 4.3

79
Q

Recall what the descent path indicator (“donut”) represents during the descent and where the pilot can see the relative position to the descent path in numerical form.

The descent path indicator (“donut”) represents the FMS ____ ______.

Vertical deviation information is shown digitally on the _____ page in the ______ field.

A

AUTO_445 FCTM 4.3

Recall what the descent path indicator (“donut”) represents during the descent and where the pilot can see the relative position to the descent path in numerical form.

The descent path indicator (“donut”) represents the FMS descent profile.

Vertical deviation information is shown digitally on the PROG page in the VDEV field.

FCTM 4.3

80
Q

AUTO_450 FCTM 4.3

Recall what is indicated by the blue level-off arrow while performing a Managed Descent.

Where the _____ _______ will reach the altitude selected on the FCU.

It does not necessarily represent where the aircraft will reach the _____ altitude unless the aircraft is on the _______.

A

AUTO_450 FCTM 4.3

Recall what is indicated by the blue level-off arrow while performing a Managed Descent.

Where the descent profile will reach the altitude selected on the FCU.

It does not necessarily represent where the aircraft will reach the FCU altitude unless the aircraft is on the profile.

FCTM 4.3

81
Q

AUTO_455 FCTM 4.3

Recall the hazard of descending to an altitude below 10,000’ MSL with a selected speed or greater than 250 knots.

A

AUTO_455 FCTM 4.3

Recall the hazard of descending to an altitude below 10,000’ MSL with a selected speed or greater than 250 knots.

The 250 knot speed limit at 10,000’ is not honored.

FCTM 4.3

82
Q

AUTO_460 FCTM 4.3

Recall the basic description of the Open Descent mode and the relationship between an Open Descent and the calculated descent path.

In the Open Descent (OP DES) mode, the FMS uses ____ _____ and varies the ____ to maintain the target ______ (selected or managed).

An Open Descent does not follow the _______ descent path (as does Managed Descent).

A

AUTO_460 FCTM 4.3

Recall the basic description of the Open Descent mode and the relationship between an Open Descent and the calculated descent path.

In the Open Descent (OP DES) mode, the FMS uses idle thrust and varies the pitch to maintain the target airspeed (selected or managed).

An Open Descent does not follow the calculated descent path (as does Managed Descent).

FCTM 4.3

83
Q

AUTO_465 FCTM 4.3

Recall the thrust requested and vertical mode engaged when an altitude below the aircraft is put in the altitude window of the FCU and the altitude knob is pulled.

A

AUTO_465 FCTM 4.3

Recall the thrust requested and vertical mode engaged when an altitude below the aircraft is put in the altitude window of the FCU and the altitude knob is pulled.

Idle thrust (THR IDLE) and

Open Descent (OP DES).

FCTM 4.3

84
Q

AUTO_470 FCTM 4.3

Recall the effect on the descent if a lower speed is selected while in an Open Descent.

Selecting a slower airspeed ______ the descent and ______ the level-off point.

A

AUTO_470 FCTM 4.3

Recall the effect on the descent if a lower speed is selected while in an Open Descent.

Selecting a slower airspeed shallows the descent and extends the level-off point.

FCTM 4.3

85
Q

AUTO_475 FCTM 4.3

Recall whether the descent path indicator (“donut”) is available during an Open Descent.

The descent path indicator on the PFD ___ ____ available during an Open Descent if the aircraft’s path is within _ nm of the ______ descent path, but references the _______ Descent profile.

A

AUTO_475 FCTM 4.3

Recall whether the descent path indicator (“donut”) is available during an Open Descent.

The descent path indicator on the PFD will be available during an Open Descent if the aircraft’s path is within 4 nm of the managed descent path, but references the Managed Descent profile.

FCTM 4.3

86
Q

AUTO_480 FCTM 4.3

Recall how altitude constraints are treated during an Open Descent.

A

AUTO_480 FCTM 4.3

Recall how altitude constraints are treated during an Open Descent.

In Open Descent, the FMS constraints are not honored.

FCTM 4.3

87
Q

AUTO_485 FCTM 4.3

Recall the caution with regard to hand-flying during an Open Descent.

The ______ _______ pitch guidance must be followed when hand flying the aircraft.

The target ________ will not be maintained if the pitch guidance is not followed.

A

AUTO_485 FCTM 4.3

Recall the caution with regard to hand-flying during an Open Descent.

The flight director pitch guidance must be followed when hand flying the aircraft.

The target airspeed will not be maintained if the pitch guidance is not followed.

FCTM 4.3

88
Q

AUTO_490 FCTM 4.3

Understand the effect of extending speedbrakes when performing an Open Descent.

In OP DES, extending the speedbrakes will _______ the descent rate.

This will cause the level-off arrow to move _____ to the aircraft on the ND.

A

AUTO_490 FCTM 4.3

Understand the effect of extending speedbrakes when performing an Open Descent.

In OP DES, extending the speedbrakes will increase the descent rate.

This will cause the level-off arrow to move closer to the aircraft on the ND.

FCTM 4.3

89
Q

AUTO_495 FCTM 4.3

Recall the basic description of the V/S descent mode.

In the Vertical Speed (V/S) descent mode, the FMS commands a _____ to maintain the selected ____ _______ and varies the thrust to maintain the target _______.

A

AUTO_495 FCTM 4.3

Recall the basic description of the V/S descent mode.

In the Vertical Speed (V/S) descent mode, the FMS commands a pitch to maintain the selected vertical speed and varies the thrust to maintain the target airspeed.

FCTM 4.3

90
Q

AUTO_500 FCTM 4.3

Recall how altitude constraints are treated during the Vertical Speed descent mode.

A

AUTO_500 FCTM 4.3

Recall how altitude constraints are treated during the Vertical Speed descent mode.

In the Vertical Speed mode, FMS altitude and speed constraints are not honored.

FCTM 4.3

91
Q

AUTO_505 V2 22_30.70

Recall what occurs if the V/S or FPA knob is pushed during a descent.

The autoflight system commands an ____ ____-____ by engaging the V/S or FPA mode with a target of ______.

A

AUTO_505 V2 22_30.70

Recall what occurs if the V/S or FPA knob is pushed during a descent.

The autoflight system commands an immediate level-off by engaging the V/S or FPA mode with a target of zero.

V2 22_30.70

92
Q

AUTO_510 V2 22_30.70

Recall the thrust setting used by the autothrust system and the column 1 indication in the FMA when the V/S mode is engaged during a descent.

A

AUTO_510 V2 22_30.70

Recall the thrust setting used by the autothrust system and the column 1 indication in the FMA when the V/S mode is engaged during a descent.

Variable thrust: SPEED (or MACH)

V2 22_30.70

93
Q

AUTO_515 FCTM 4.3

Recall what occurs if an excessive V/S is selected during a descent.

If the selected V/S is too steep to maintain the target airspeed at idle thrust, the airspeed will ________ until approaching _______.

At this point the selected V/S automatically _______ to avoid ________ the limiting speed.

A

AUTO_515 FCTM 4.3

Recall what occurs if an excessive V/S is selected during a descent.

If the selected V/S is too steep to maintain the target airspeed at idle thrust, the airspeed will increase until approaching VMAX.

At this point the selected V/S automatically shallows to avoid exceeding the limiting speed.

FCTM 4.3

94
Q

AUTO_520 V2 22_30.70

Recall the target speed used for descent when EXPED pb is pushed during a descent and whether the 250-knot speed limit at 10,000’ or constraints are considered when descending in the EXP DES mode.

Target speed is _____ knots or 0._ Mach.

When the EXP DES mode is active, the system ______ speed limits (250 kts at 10,000’ MSL).

When the EXP DES mode is active, the system ______ speed and altitude constraints.

A

AUTO_520 V2 22_30.70

Recall the target speed used for descent when EXPED pb is pushed during a descent and whether the 250-knot speed limit at 10,000’ or constraints are considered when descending in the EXP DES mode.

Target speed is 340 knots or 0.8 Mach.

When the EXP DES mode is active, the system disregards speed limits (250 kts at 10,000’ MSL).

When the EXP DES mode is active, the system disregards speed and altitude constraints.

V2 22_30.70

95
Q

AUTO_525 V2 22_30.70

Recall what thrust setting and column 1 and 2 FMA indications are expected when descending in the EXP DES mode.

A

AUTO_525 V2 22_30.70

Recall what thrust setting and column 1 and 2 FMA indications are expected when descending in the EXP DES mode.

• Idle thrust; THR IDLE, EXP DES

V2 22_30.70

96
Q

AUTO_530 V2 22_30.75

Recall the effect of changing the FCU altitude while ALT* is active in column 2 of the FMA.

A

AUTO_530 V2 22_30.75

Recall the effect of changing the FCU altitude while ALT* is active in column 2 of the FMA.

The active vertical mode changes to V/S with the selected vertical speed being the vertical speed that existed at the time of the change.

V2 22_30.75

97
Q

AUTO_535 (Approach) FCTM 1.5

Recall what the managed speed target becomes after activating the approach phase.

Once the approach phase is activated, the FMS sets managed speed to the ____ ____ ____ for the ______ flap configuration (normally FLAPS 3 or FULL), _______ of the current flap setting.

A

AUTO_535 (Approach) FCTM 1.5

Recall what the managed speed target becomes after activating the approach phase.

Once the approach phase is activated, the FMS sets managed speed to the final approach speed for the landing flap configuration (normally FLAPS 3 or FULL), regardless of the current flap setting.

FCTM 1.5

98
Q

AUTO_540 FCTM 1.5

Recall the lowest speed the autothrust will command after activating the approach phase.

The autothrust will not command a slower speed than the minimum ______ ______ for the ______ flap setting when in _______ speed.

A

AUTO_540 FCTM 1.5

Recall the lowest speed the autothrust will command after activating the approach phase.

The autothrust will not command a slower speed than the minimum maneuvering speed for the existing flap setting when in managed speed.

FCTM 1.5

99
Q

AUTO_545 V2 APP 31.40

Recall the meanings of the F and S airspeed indications on the speed tape.

S Speed is the Minimum _____ Retraction Speed (green letter _), and appears when flap selector is in position _.

F Speed is the Minimum ____ Retraction speed (green letter _), and appears when the flap selector is in position _ or _.

V2 31.40

A

AUTO_545 V2 APP 31.40

Recall the meanings of the F and S airspeed indications on the speed tape.

S Speed is the Minimum Slat Retraction Speed (green letter S), and appears when flap selector is in position 1.

F Speed is the Minimum Flap Retraction speed (green letter F), and appears when the flap selector is in position 2 or 3.

V2 31.40

100
Q

AUTO_550 V2 22_30.90

Recall the purpose of Ground Speed Mini.

Ground Speed Mini ensures the ______ of the aircraft is maintained above a minimum level when _______ conditions vary during the approach.

A

AUTO_550 V2 22_30.90

Recall the purpose of Ground Speed Mini.

Ground Speed Mini ensures the energy of the aircraft is maintained above a minimum level when wind conditions vary during the approach.

V2 22_30.90

101
Q

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

During level flight, ATC provides a heading to intercept the localizer.

The PF pushes the LOC pb:

A

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

During level flight, ATC provides a heading to intercept the localizer. The PF pushes the LOC pb.

102
Q

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

The localizer is intercepted:

A

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

The localizer is intercepted:

103
Q

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

After intercepting the localizer, ATC provides the ILS approach clearance and the PF pushes the APPR pb and the second AP

A

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

After intercepting the localizer, ATC provides the ILS approach clearance and the PF pushes the APPR pb and the second AP

104
Q

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

The glideslope is intercepted:

A

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

The glideslope is intercepted:

105
Q

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

The aircraft passes approximately 400’ RA during the ILS approach:

A

AUTO_555 APP FCTM 5.2

Recall the columns 1, 2, 3, 4 and 5 indications on the FMA during an ILS approach.

The aircraft passes approximately 400’ RA during the ILS approach:

106
Q

AUTO_560 FCTM 5.2

Recall if the GS mode can be active before the LOC mode is active.

The glideslope may be _______ before the localizer and may be captured from either ____ or ______.

A

AUTO_560 FCTM 5.2

Recall if the GS mode can be active before the LOC mode is active.

The glideslope may be captured before the localizer and may be captured from either above or below.

FCTM 5.2

107
Q

AUTO_565 FCTM 5.2

Recall whether the aircraft levels-off when approaching the FCU altitude while descending in the GS mode:

A

AUTO_565 FCTM 5.2

Recall whether the aircraft levels-off when approaching the FCU altitude while descending in the GS mode.

The FCU altitude is ignored when descending in the GS mode.

FCTM 5.2

108
Q

AUTO_570 APP FCTM 5.2

Recall the columns 1, 2, and 3 indications on the FMA during an autoland from an ILS approach.

At 50’ RA:

A

AUTO_570 APP FCTM 5.2

Recall the columns 1, 2, and 3 indications on the FMA during an autoland from an ILS approach.

At 50’ RA:

109
Q

AUTO_570 APP FCTM 5.2

Recall the columns 1, 2, and 3 indications on the FMA during an autoland from an ILS approach.

At 20’ RA

A

AUTO_570 APP FCTM 5.2

Recall the columns 1, 2, and 3 indications on the FMA during an autoland from an ILS approach.

At 20’ RA

110
Q

AUTO_570 APP FCTM 5.2

Recall the columns 1, 2, and 3 indications on the FMA during an autoland from an ILS approach.

At touchdown – thrust levers have been moved to IDLE stop:

A

AUTO_570 APP FCTM 5.2

Recall the columns 1, 2, and 3 indications on the FMA during an autoland from an ILS approach.

At touchdown – thrust levers have been moved to IDLE stop:

111
Q

AUTO_575 APP FCTM 5.3

Recall the column 2 and 3 indications on the FMA during an RNAV approach.

During level flight, ATC provides “direct to” clearance to a waypoint on the RNAV approach:

A

AUTO_575 APP FCTM 5.3

Recall the column 2 and 3 indications on the FMA during an RNAV approach.

During level flight, ATC provides “direct to” clearance to a waypoint on the RNAV approach.

112
Q

AUTO_575 APP FCTM 5.3

Recall the column 2 and 3 indications on the FMA during an RNAV approach.

When the TO waypoint is the Final Descent Point (FDP) the PF pushes the ______ pb:

A

AUTO_575 APP FCTM 5.3

Recall the column 2 and 3 indications on the FMA during an RNAV approach.

When the TO waypoint is the Final Descent Point (FDP) the PF pushes the APPR pb:

113
Q

AUTO_575 APP FCTM 5.3

Recall the column 2 and 3 indications on the FMA during an RNAV approach.

When the V/DEV is within ____ feet, FINAL APP will engage and vertical guidance will follow the brick.

A

AUTO_575 APP FCTM 5.3

Recall the column 2 and 3 indications on the FMA during an RNAV approach.

When the V/DEV is within 250 feet, FINAL APP will engage and vertical guidance will follow the brick.

114
Q

AUTO_580 FCTM 5.7

Recall the FMA columns 1, 2 and 3 indications when the thrust levers are set to TOGA on a Go-Around with the flaps/slats extended.

Column 1:

Column 2:

Column 3:

A

AUTO_580 FCTM 5.7

Recall the FMA columns 1, 2 and 3 indications when the thrust levers are set to TOGA on a Go-Around with the flaps/slats extended.

Column 1: MAN TOGA
Column 2: SRS active (green) ALT armed (blue) Column 3: Initially GA TRK, then NAV

FCTM 5.7

115
Q

AUTO_585 FCTM 5.7

Recall the FMA column 3 indications when the thrust levers are set to TOGA on a Go- Around with the flaps/slats extended, no heading preselected, and no missed approach in the FMS.

A

AUTO_585 FCTM 5.7

Recall the FMA column 3 indications when the thrust levers are set to TOGA on a Go- Around with the flaps/slats extended, no heading preselected, and no missed approach in the FMS.

GA TRK

FCTM 5.7

116
Q

AUTO_590 FCTM 5.7

Recall the FMA column 2 indications at Thrust Reduction Altitude on a Go-Around.

__ ___ active (green)

____ armed (blue)

A

AUTO_590 FCTM 5.7

Recall the FMA column 2 indications at Thrust Reduction Altitude on a Go-Around.

OP CLB active (green)

ALT armed (blue)

FCTM 5.7

117
Q

AUTO_595 FCTM 5.7

Recall what the lateral and vertical mode will be if Go-Around is initiated with the flaps/slats up.

A

AUTO_595 FCTM 5.7

Recall what the lateral and vertical mode will be if Go-Around is initiated with the flaps/slats up.

Current lateral and vertical modes remain engaged.

FCTM 5.7

118
Q

AUTO_600 FCTM 5.7

Describe what the flight directors will do if they are OFF and a Go-Around is initiated with the flaps/slats extended.

The flight directors will automatically engage in ____ and ____ or (___ and ___ ____ if FMS missed approach unavailable).

A

AUTO_600 FCTM 5.7

Describe what the flight directors will do if they are OFF and a Go-Around is initiated with the flaps/slats extended.

The flight directors will automatically engage in SRS and NAV or (SRS and GA TRK if FMS missed approach unavailable).

FCTM 5.7

119
Q

AUTO_605 FCTM 5.7

Recall why altitude constraints are not honored during a Go-Around:

At acceleration altitude the vertical mode changes to __ ___.

OP CLB ___ ____ ____ altitude constraints.

A

AUTO_605 FCTM 5.7

Recall why altitude constraints are not honored during a Go-Around.

At acceleration altitude the vertical mode changes to OP CLB.

OP CLB does not honor altitude constraints.

FCTM 5.7

120
Q

AUTO_610 FCTM 5.7

Describe what happens to the autothrust system if a Go-Around is initiated with the flaps/slats extended while the is autothrust off.

With TOGA selected the autothrust will ____

(_/___ in blue in FMA column _).

A

AUTO_610 FCTM 5.7

Describe what happens to the autothrust system if a Go-Around is initiated with the flaps/slats extended while the is autothrust off.

With TOGA selected the autothrust will arm

(A/THR in blue in FMA column 5).

FCTM 5.7

121
Q

AUTO_615 FCTM 5.7

Recall the target speed during a Go-Around with SRS as the active vertical mode:

A

AUTO_615 FCTM 5.7

Recall the target speed during a Go-Around with SRS as the active vertical mode.

VAPP or current speed whichever is higher.

FCTM 5.7

122
Q

AUTO_620 FCTM 5.7

Recall the color of the missed approach portion of the flight plan when displayed on the NAV display prior to becoming the active phase.

A

AUTO_620 FCTM 5.7

Recall the color of the missed approach portion of the flight plan when displayed on the NAV display prior to becoming the active phase.

Blue

FCTM 5.7

123
Q

AUTO_625 FCTM 5.7

Describe what happens to the flight plan following a missed approach.

TOGA detent selected (with flaps/slats extended): The previous approach is automatically __-_____ into the F-PLN after the current missed approach procedure without a VIA (i.e., only the common portion of the approach).

TOGA detent not selected:

The flight plan will _______ at the end of the missed approach procedure, and the previous approach will not be _________.

The pilot must re-enter the _______ as a new ______ and re-insert the _______.

A

AUTO_625 FCTM 5.7

Describe what happens to the flight plan following a missed approach.

TOGA detent selected (with flaps/slats extended): The previous approach is automatically re-inserted into the F-PLN after the current missed approach procedure without a VIA (i.e., only the common portion of the approach).

TOGA detent not selected:

The flight plan will terminate at the end of the missed approach procedure, and the previous approach will not be re-inserted.

The pilot must re-enter the destination as a new destination and re-insert the approach

FCTM 5.7

124
Q

AUTO_630 FCTM 5.7

Recall the target speed at acceleration altitude on a Go-Around.

A

AUTO_630 FCTM 5.7

Recall the target speed at acceleration altitude on a Go-Around.

Green Dot

FCTM 5.7