CH06 A330 FLT MGMT Flashcards
FLTMGT_01 Understand the control functions and indications on the ADIRS panel.
- 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
FLTMGT_01 Understand the control functions and indications on the ADIRS panel.
- 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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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.
- ADIRU ________ can be selected as a backup for either pilot’s instruments by using the:
VOL. II,31.2.5.6
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.
- ADIRU 3 can be selected as a backup for either pilot’s instruments by using the:
VOL. II,31.2.5.6
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
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
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
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
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
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
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)
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)
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 ________)
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)
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
