Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

A-330 Learning Objectives Document September 22, 2021 > CH06 A330 FLT MGMT > Flashcards

CH06 A330 FLT MGMT Flashcards

1
Q

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

  1. ON BAT Light
  • The ON BAT light illuminates when one or more ______ is supplied only by the aircraft ________.
  • It also illuminates for a few seconds at the beginning of a ________ ______ as part of the self test.

VOL. II, 34.2.12.2.7

A

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

  1. ON BAT Light
  • The ON BAT light illuminates when one or more IRs is supplied only by the aircraft batteries.
  • It also illuminates for a few seconds at the beginning of a full alignment as part of the self test.

VOL. II, 34.2.12.2.7

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

2. IR pbs
FAULT light - A fault is detected in the respective ______.

  • Illuminated steady - The respective IR is ________.
  • Flashing - Attitude and heading information may be recovered in ________ mode.
  • OFF - If the pb is selected OFF, the OFF light ________ and the respective IR is selected off, without disabling the ________ portion of the ADIRU.

VOL. II, 34.2.12.2.7

A

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

2. IR pbs
FAULT light - A fault is detected in the respective IR.

  • Illuminated steady - The respective IR is lost.
  • Flashing - Attitude and heading information may be recovered in ATT mode.
  • OFF - If the pb is selected OFF, the OFF light illuminates and the respective IR is selected off, without disabling the ADR portion of the ADIRU.

VOL. II, 34.2.12.2.7

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

3. Mode Selectors

  • OFF - Both the ________ and ________ of the respective IRU are ________.
  • NAV - The ________ operating position.
  • ATT - ________ mode.
    • ______ position information is lost.
    • In flight alignment is only possible in ________ mode.

VOL. II, 34.2.12.2.7

A

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

3. Mode Selectors

  • OFF - Both the IR and ADR of the respective IRU are unpowered.
  • NAV - The normal operating position.
  • ATT - Attitude mode.
    • IR position information is lost.
    • In flight alignment is only possible in ATT mode.

VOL. II, 34.2.12.2.7

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

4. ADR pbs

  • FAULT light illuminated - A fault is detected in the respective ________.
  • OFF - If the pb is selected OFF, the OFF light illuminates and the respective ________ is selected off, without disabling the______ portion of the ADIRU
A

FLTMGT_01 Understand the control functions and indications on the ADIRS panel.

4. ADR pbs

  • FAULT light illuminated - A fault is detected in the respective ADR.
  • OFF - If the pb is selected OFF, the OFF light illuminates and the respective ADR is selected off, without disabling the IR portion of the ADIRU

VOL. II, 34.2.12.2.7

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

FLTMGT_02 Describe how to accomplish a full ADIRS alignment.

A green ____ ______ ______ memo is displayed on the ______ along with the approximate time until alignment is complete and navigation is possible (e.g., ____ ______ ______ > 7 MIN).

VOL. II, 34.2.13.2

A

FLTMGT_02 Describe how to accomplish a full ADIRS alignment.

A green IRS IN ALIGN memo is displayed on the UPPER E/WD along with the approximate time until alignment is complete and navigation is possible (e.g., IRS IN ALIGN > 7 MIN).

VOL. II, 34.2.13.2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

FLTMGT_03 Describe the errors that may be presented during an ADIRS alignment.

  • The ______ ______ ______ along with the approximate time (e.g., ______ ______ ______ > 7 MIN) appears in _________ if the engines are running.

VOL. II, 34.2.13.6

A

FLTMGT_03 Describe the errors that may be presented during an ADIRS alignment.

  • The IRS IN ALIGN along with the approximate time (e.g., IRS IN ALIGN > 7 MIN) appears in amber if the engines are running.

VOL. II, 34.2.13.6

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

FLTMGT_03 Describe the errors that may be presented during an ADIRS alignment.

  • Alignment errors can occur due to:
  • excessive aircraft ________ during alignment,
  • or a position ________.
  • The green _____ _____ ____memo on the E/WD flashes during the alignment process if an alignment problem exists:
    • If excessive motion is detected, the alignment is automatically ________.
    • Each IRU memorizes the computed present position when it is _______._
    • If a significant ________ exists between the position entered on INIT page A and the last ________ position, the ______ ______ prompt is displayed again on INIT page A and the position must be______.

VOL. II, 34.2.13.6

A

FLTMGT_03 Describe the errors that may be presented during an ADIRS alignment.

  • Alignment errors can occur due to:
  • excessive aircraft movement during alignment,
  • or a position disagreement.
  • The green IRS IN ALIGN memo on the E/WD flashes during the alignment process if an alignment problem exists:
    • If excessive motion is detected, the alignment is automatically restarted.
    • Each IRU memorizes the computed present position when it is shutdown.
    • If a significant difference exists between the position entered on INIT page A and the last memorized position, the ALIGN IRS prompt is displayed again on INIT page A and the position must be re-entered.

VOL. II, 34.2.13.6

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

FLTMGT_04 Describe the EFIS data switching process.

Normally, ADIRU 1 supplies data for:

  • the ______ ________,
  • ________,
  • ________,
  • and ATC transponder _______.

ADIRU 2 supplies data for:

  • the______ ______ ______,
  • ______,
  • and ATC transponder ____.

ADIRU 3 normally does not provide information to the instrument system, and serves as a backup for ______ 1 or 2.

VOL. II,31.2.5.6

A

FLTMGT_04 Describe the EFIS data switching process.

Normally, ADIRU 1 supplies data for:

  • the Captain’s PFD,
  • ND,
  • DDRMI,
  • and ATC transponder 1.

ADIRU 2 supplies data for:

  • the first officer’s PFD,
  • ND,
  • and ATC transponder 2.

ADIRU 3 normally does not provide information to the instrument system, and serves as a backup for ADIRU 1 or 2.

VOL. II,31.2.5.6

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

FLTMGT_04 Describe the EFIS data switching process.

  • Should a failure of either heading and attitude data, or air data be indicated on the EFIS:
    • ADIRU ________ can be selected as a backup for either pilot’s instruments by using the:
      • ______ ______ and
      • ______ ______ selectors.

VOL. II,31.2.5.6

A

FLTMGT_04 Describe the EFIS data switching process.

  • Should a failure of either heading and attitude data, or air data be indicated on the EFIS:
    • ADIRU 3 can be selected as a backup for either pilot’s instruments by using the:
      • ATT HDG and
      • AIR DATA selectors.

VOL. II,31.2.5.6

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

FLTMGT_04 Describe the EFIS data switching process.

Should a failure of either heading and attitude data, or air data be indicated on the EFIS:

  • Selecting CAPT on 3 or F/O on 3 will transfer the data source from the normal source to _________ ____.
  • In case of total failure of ADIRU 1 or 2, both the ________ ________and ___ ____ selectors will need to be selected to:
    • CA ON ____ or
    • F/O ON ____ as appropriate.

VOL. II,31.2.5.6

A

FLTMGT_04 Describe the EFIS data switching process.

Should a failure of either heading and attitude data, or air data be indicated on the EFIS:

  • Selecting CAPT on 3 or F/O on 3 will transfer the data source from the normal source to ADIRU 3.
  • In case of total failure of ADIRU 1 or 2, both the AIR DATA and ATT HDG selectors will need to be selected to:
    • CA ON 3 or
    • F/O ON 3 as appropriate.

VOL. II,31.2.5.6

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

FLTMGT_05 Recall what flight instrument data is AD information vs IR information.

Air Data
• PFD

  • Indicated ______/______
  • Barometric ________
  • ______ ______velocity (barometric)

• ND

  • ________ Speed (______)

• SD

  • ______ ______ ______ (________) and ________ __ __________ (______)

V2 34.2.12.2.3
34.2.12.2.5

A

FLTMGT_05 Recall what flight instrument data is AD information vs IR information.

Air Data
• PFD

  • Indicated airspeed/Mach
  • Barometric altitude
  • Backup vertical velocity (barometric)

• ND

  • True Air Speed (TAS)

• SD

  • Total Air Temperature (TAT) and Static Air Temperature (SAT)
  • *V2 34.2.12.2.3**
    34. 2.12.2.5
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

FLTMGT_05 Recall what flight instrument data is AD information vs IR information.

Inertial Reference:

• PFD

  • _A_______
  • _V_______velocity
  • F______ P______ vector
  • _H_______ (______ or ______)
  • _T_______

• ND

  • _H_______ (true or magnetic)
  • ______ wind direction and velocity
  • W______ vector relative to the aircraft H________ (displayed as an arrow on the ________)
  • _T_______
  • G______ ______
  • _P_______ (refined and provided via the FMS)

• DDRMI

  • ________ (true or magnetic)

V2
34.2.12.2.5

A

FLTMGT_05 Recall what flight instrument data is AD information vs IR information.

Inertial Reference:

• PFD

  • Attitude
  • Vertical velocity
  • Flight path vector
  • Heading (true or magnetic)
  • Track

• ND

  • Heading (true or magnetic)
  • True wind direction and velocity
  • Wind vector relative to the aircraft heading (displayed as an arrow on the ND)
  • Track
  • Ground speed
  • Position (refined and provided via the FMS)

• DDRMI

  • Heading (true or magnetic)

V2
34.2.12.2.5

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

FLTMGT_05 Recall what flight instrument data is AD information vs IR information. V2 34.2.12.2.3
34.2.12.2.5

Inertial Reference

• ND

  • o ________g (true or magnetic)
  • o True ________ direction and ________
  • o Wind ________ relative to the aircraft ________ (displayed as an arrow on the ND)
  • o ________
  • o ________ speed
  • o ________ (refined and provided via the FMS)

• DDRMI

  • o _________ (true or magnetic)
A

FLTMGT_05 Recall what flight instrument data is AD information vs IR information. V2 34.2.12.2.3
34.2.12.2.5

Inertial Reference
• ND

  • o Heading (true or magnetic)
  • o True wind direction and velocity
  • o Wind vector relative to the aircraft heading (displayed as an arrow on the ND)
  • o Track
  • o Ground speed
  • o Position (refined and provided via the FMS)

• DDRMI

  • o Heading (true or magnetic)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

FLTMGT_05 Recall what flight instrument data is AIR DATA AD information vs IR information. V2 34.2.12.2.3
34.2.12.2.5

Inertial Reference
• DDRMI

  • o ___________ (_______ or ________)
A

FLTMGT_05 Recall what flight instrument data is AIR DATA AD information vs IR information. V2 34.2.12.2.3
34.2.12.2.5

Inertial Reference
• DDRMI

  • o Heading (true or magnetic)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

FLTMGT_06 Describe how GPS is integrated into the navigational systems.

The aircraft has ________ GPS receivers.

  • Each GPS receiver is integrated, along with the____ receivers, in a modular avionics unit called the:
    • ______ ______ ______ (MMR).
  • Each MMR processes the data received and transmits it to its associated ________.
    • The ________ then calculates a combined ______-______ position (the GPIRS position).
    • The FMS uses the ______-______ position whenever GPS information is available.
    • In normal operation, ADIRU 1 and 3 are supplied by ________
      • ADIRU 2 is supplied by ________.
    • If one MMR receiver fails, the remaining receiver ________ supplies all ________

VOL. II, 34.2.14.1

A

FLTMGT_06 Describe how GPS is integrated into the navigational systems.

The aircraft has two GPS receivers.

  • Each GPS receiver is integrated, along with the ILS receivers, in a modular avionics unit called the:
    • Multi Mode Receiver (MMR).
  • Each MMR processes the data received and transmits it to its associated ADIRU.
    • The ADIRU then calculates a combined GPS-IRS position (the GPIRS position).
    • The FMS uses the GP-IRS position whenever GPS information is available.
    • In normal operation, ADIRU 1 and 3 are supplied by MMR 1
      • ADIRU 2 is supplied by MMR 2.
    • If one MMR receiver fails, the remaining receiver automatically supplies all ADIRUs

VOL. II, 34.2.14.1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

FLTMGT_06 Describe how GPS is integrated into the navigational systems.

Multi Mode Receiver (MMR):

  • Each MMR processes the data received and transmits it to its associated ________.
  • The ________ then calculates a combined ______-______ position (the ________ position).

The FMS uses the ______-______ position whenever GPS information is available.

  • In normal operation, ______ __ and __ are supplied by MMR 1
  • and ______ __ is supplied by MMR 2.
  • If one ________ receiver fails, the remaining receiver automatically supplies all ADIRUs

VOL. II, 34.2.14.1

A

FLTMGT_06 Describe how GPS is integrated into the navigational systems.

Multi Mode Receiver (MMR):

  • Each MMR processes the data received and transmits it to its associated ADIRU.
  • The ADIRU then calculates a combined GPS-IRS position (the GPIRS position).

The FMS uses the GP-IRS position whenever GPS information is available.

  • In normal operation, ADIRU 1 and 3 are supplied by MMR 1
  • and ADIRU 2 is supplied by MMR 2.
  • If one MMR receiver fails, the remaining receiver automatically supplies all ADIRUs

VOL. II, 34.2.14.1

17
Q

FLTMGT_06 Describe how GPS is integrated into the navigational systems. VOL. II, 34.2.14.1

The FMS uses the GP-IRS position whenever GPS information is available.

In normal operation, ADIRU 1 and 3 are supplied by MMR 1 and ADIRU 2 is supplied by MMR 2.

If one MMR receiver fails, the remaining receiver automatically supplies all ADIRUs

A

FLTMGT_06 Describe how GPS is integrated into the navigational systems. VOL. II, 34.2.14.1

The FMS uses the GP-IRS position whenever GPS information is available.

In normal operation, ADIRU 1 and 3 are supplied by MMR 1 and ADIRU 2 is supplied by MMR 2.

If one MMR receiver fails, the remaining receiver automatically supplies all ADIRUs

18
Q

FLTMGT_06 Describe how GPS is integrated into the navigational systems.

Note: Do not enter the gate coordinates unless GPS is inoperative.

  • When GPS is operative, the ADIRUs calculate a _____–_____ hybrid position which is more accurate than the gate position.

VOL. II, 34.2.14.1

A

FLTMGT_06 Describe how GPS is integrated into the navigational systems.

Note: Do not enter the gate coordinates unless GPS is inoperative.

  • When GPS is operative, the ADIRUs calculate a GPS-IR hybrid position which is more accurate than the gate position.

VOL. II, 34.2.14.1

19
Q

FLTMGT_07 Describe the Polar navigation features.

  • Due to ______ ______ anomalies, only true heading is available in the polar regions.
  • True heading may be selected for display at any time using the ______ ______ pb on the forward instrument panel.
  • If TRUE is not selected when approaching the polar regions, the _____ _____ _____message is displayed on the _____.
  • If TRUE is not selected manually, a switchover to TRUE will occur ________ accompanied by an ________ message.
  • VOL. II, 34.4.4.15
A

FLTMGT_07 Describe the Polar navigation features.

  • Due to magnetic field anomalies, only true heading is available in the polar regions.
  • True heading may be selected for display at any time using the NORTH REF pb on the forward instrument panel.
  • If TRUE is not selected when approaching the polar regions, the SELECT TRU REF message is displayed on the ND.
  • If TRUE is not selected manually, a switchover to TRUE will occur automatically accompanied by an ECAM message.
  • VOL. II, 34.4.4.15
20
Q

FLTMGT_07 Describe the Polar navigation features.

Caution: If the heading reference is allowed to switch over automatically, an ________ disconnect may occur.

  • This is because a heading ________ may occur if all ________ do not reach the switch over ________ simultaneously.

VOL. II, 34.4.4.15

A

FLTMGT_07 Describe the Polar navigation features.

Caution: If the heading reference is allowed to switch over automatically, an autopilot disconnect may occur.

  • This is because a heading disagreement may occur if all IRUs do not reach the switch over latitude simultaneously.

VOL. II, 34.4.4.15

21
Q

FLTMGT_07 Describe the Polar navigation features. VOL. II, 34.4.4.15

When selected heading references on the PFDs, NDs, and DDRMI are relative to true north:

  • _______is displayed above the _______ and _______ heading scales.

VOL. II, 34.4.4.15

A

FLTMGT_07 Describe the Polar navigation features. VOL. II, 34.4.4.15

When selected heading references on the PFDs, NDs, and DDRMI are relative to true north:

  • TRU is displayed above the PFD and ND heading scales.

VOL. II, 34.4.4.15

22
Q

FLTMGT_07 Describe the Polar navigation features.

  • The heading reference will not ____________ switch back to _______ when magnetic heading information becomes available.
    • Selection of ________ should be delayed until clear of the polar region.

VOL. II, 34.4.4.15

A

FLTMGT_07 Describe the Polar navigation features.

  • The heading reference will not automatically switch back to MAG when magnetic heading information becomes available.
    • Selection of MAG should be delayed until clear of the polar region.

VOL. II, 34.4.4.15

23
Q

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

GPS PRIMARY:

  • GPS PRIMARY is displayed when the ________ navigation mode is ______ ______
  • When GPS PRIMARY is not available or navigation mode is not GPS/IRS, the field is ________.
  • The MCDU scratchpad and ______ displays the message ______ ______ when the field first appears
    • and _______ ______ _______ when the field becomes blank.
  • VOL. II, 34.6.8.1. 11-14
A

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

GPS PRIMARY:

  • GPS PRIMARY is displayed when the FMS navigation mode is GPS PRIMARY.
  • When GPS PRIMARY is not available or navigation mode is not GPS/IRS, the field is blank.
  • The MCDU scratchpad and ND displays the message GPS PRIMARY when the field first appears
    • and GPS PRIMARY LOST when the field becomes blank.
  • VOL. II, 34.6.8.1. 11-14
24
Q

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

REQUIRED:

  • The REQUIRED field displays the default value for the _____ ____________ ______ (______) level in NM for the current area or procedure.
    • The field can be modified if a different ________ value is known for the particular area or procedure.

VOL. II, 34.6.8.1. 11-14

A

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

REQUIRED:

  • The REQUIRED field displays the default value for the Required Navigation Performance (RNP) level in NM for the current area or procedure.
    • The field can be modified if a different RNP value is known for the particular area or procedure.

VOL. II, 34.6.8.1. 11-14

25
Q

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

ACCUR:

  • The ACCUR field displays the evaluation of the ________ accuracy value as compared to the ________ accuracy level.
  • If the ________ position error is equal to or ______ ______ the ________ value, the field displays ________.
  • If the error is greater than the ________ value the field displays ________.
  • VOL. II, 34.6.8.1. 11-14
A

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

ACCUR:

  • The ACCUR field displays the evaluation of the ESTIMATED accuracy value as compared to the REQUIRED accuracy level.
  • If the ESTIMATED position error is equal to or less than the REQUIRED value, the field displays HIGH.
  • If the error is greater than the REQUIRED value the field displays LOW.
  • VOL. II, 34.6.8.1. 11-14
26
Q

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

ESTIMATED:

  • The ESTIMATED field displays the current estimated ______ ______ in NM as computed by the ________.

VOL. II, 34.6.8.1. 11-14

A

FLTMGT_08 Recall where to find the navigational accuracy level in the MCDU.

ESTIMATED:

  • The ESTIMATED field displays the current estimated position error in NM as computed by the FMS.

VOL. II, 34.6.8.1. 11-14

A-330 Learning Objectives Document September 22, 2021 (16 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions