CH15 A330 WRNG Flashcards

1
Q

WRNG_01
Discuss the three levels of ECAM malfunction notifications.
The ECAM provides three levels of system malfunction notifications:

  • • _____
  • • _____
  • • _____

VOL. II, 31.4.4.2

A

WRNG_01
Discuss the three levels of ECAM malfunction notifications.
The ECAM provides three levels of system malfunction notifications:

  • Warnings
  • • Cautions
  • • Advisories

VOL. II, 31.4.4.2

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2
Q

WRNG_01
Discuss the three levels of ECAM malfunction notifications.
Warnings require __________ action.

  • The aircraft is in a dangerous condition or exceeding limit conditions (e.g., fire, stall, or overspeed condition).
  • Warnings will be accompanied by:
    • the _____ _____ _____ (_____)
    • or other failure specific _______
    • or _____ _____,
    • as well the following visual references:
  • Red_____ _____ lights or other specific _______ light
  • Red warning message on _______
  • Relevant _______ page on SD

VOL. II, 31.4.4.2

A

WRNG_01
Discuss the three levels of ECAM malfunction notifications.
Warnings require immediate action.

  • The aircraft is in a dangerous condition or exceeding limit conditions (e.g., fire, stall, or overspeed condition).
  • Warnings will be accompanied by:
    • the Continuous Repetitive Chime (CRC)
    • or other failure specific sound
    • or synthetic voice,
    • as well the following visual references:
  • Red MASTER WARN lights or other specific red light
  • Red warning message on E/WD
  • Relevant system page on SD

VOL. II, 31.4.4.2

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3
Q

WRNG_01
Discuss the three levels of ECAM malfunction notifications.

Level 2 cautions require crew _______ of the configuration or failure, but immediate action is not necessary.

This includes system failures with no direct effect on _____ _____y (e.g., hydraulic system low pressure).

Level 2 cautions will be accompanied by a _______ Chime, as well as the following visual references:

  • Amber _____ _____ light
  • Amber _______ caution message
  • Relevant _______ page on SD

VOL. II, 31.4.4.2

A

WRNG_01
Discuss the three levels of ECAM malfunction notifications.

Level 2 cautions require crew awareness of the configuration or failure, but immediate action is not necessary.

This includes system failures with no direct effect on flight safety (e.g., hydraulic system low pressure).

Level 2 cautions will be accompanied by a single Chime, as well as the following visual references:

  • Amber MASTER CAUT light
  • Amber ECAM caution message
  • Relevant system page on SD

VOL. II, 31.4.4.2

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4
Q

WRNG_01
Discuss the three levels of ECAM malfunction notifications.

Level 1 cautions include system failures that lead to a loss of _______ and only require crew _______ (e.g., single channel failure on some computers).

There are no _______ warnings for level 1 cautions, and are only displayed with an amber _______ caution message.
VOL. II, 31.4.4.2

A

WRNG_01
Discuss the three levels of ECAM malfunction notifications.

Level 1 cautions include system failures that lead to a loss of redundancy and only require crew monitoring (e.g., single channel failure on some computers).

There are no aural warnings for level 1 cautions, and are only displayed with an amber ECAM caution message.
VOL. II, 31.4.4.2

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5
Q

WRNG_01
Discuss the three levels of ECAM malfunction notifications.

Advisories draw attention to less serious system _______ which require crew _______.

  • They are associated with systems that are still within _______ but which are degrading.
  • This may be indicative of a pending _______.
  • Visual references typically include the associated _______ page on SD, with affected parameter _______ in green.

VOL. II, 31.4.4.2

A

WRNG_01
Discuss the three levels of ECAM malfunction notifications.

Advisories draw attention to less serious system degradations which require crew monitoring.

  • They are associated with systems that are still within limits but which are degrading.
  • This may be indicative of a pending failure.
  • Visual references typically include the associated System page on SD, with affected parameter pulsing in green.

VOL. II, 31.4.4.2

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6
Q

W

WRNG_02
Describe the purpose of the EMER CANC and RCL pbs.
1. EMER CANC

  • The EMER CANC (emergency cancel) key can be used to cancel _______ fault indications
    • or a _______ fault message as a result of operations with inoperative equipment (i.e., MEL).

Pushing the EMER CANC key for WARNINGS will:

  • Cancels the _______ warning for as long as the condition exists
  • Extinguishes the _____ _____ lights
  • Does not affect the _______ display (the message remains displayed)

VOL. II, 31.4.1.6

A

WRNG_02
Describe the purpose of the EMER CANC and RCL pbs.
1. EMER CANC

  • The EMER CANC (emergency cancel) key can be used to cancel spurious fault indications
    • or a recurring fault message as a result of operations with inoperative equipment (i.e., MEL).

Pushing the EMER CANC key for WARNINGS will:

  • Cancels the aural warning for as long as the condition exists
  • Extinguishes the MASTER WARN lights
  • Does not affect the ECAM display (the message remains displayed)

VOL. II, 31.4.1.6

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7
Q

WRNG_02
Describe the purpose of the EMER CANC and RCL pbs.
1. EMER CANC

Pushing the EMER CANC key for CAUTIONS will:

  • Cancel any present _______ for the rest of the flight including
    • _______,
    • _____ _____ lights,
    • _______ message).
      • The ECAM message is moved to the _______ page, under _________ _________.
  • • Automatically calls up the _______ page which displays ________ _________ and the _______ of the failure that is inhibited.

VOL. II, 31.4.1.6

A

WRNG_02
Describe the purpose of the EMER CANC and RCL pbs.
1. EMER CANC

Pushing the EMER CANC key for cautions will:

  • Cancels any present CAUTIONS for the rest of the flight
    • including chime,
    • MASTER CAUT lights,
    • ECAM message).
      • The ECAM message is moved to the STATUS page, under CANCELLED CAUTION.
  • • Automatically calls up the STATUS page which displays CANCELLED CAUTION and the title of the failure that is inhibited.

VOL. II, 31.4.1.6

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8
Q

WRNG_02
Describe the purpose of the EMER CANC and RCL pbs.

  1. RCL
  • The RCL (recall) key allows the crew to call up _______ messages, _______ messages, and the _______ page that may have been suppressed by the activation of the _______ key or flight phase related inhibition.
  • If there are no suppressed warnings or cautions the E/WD displays _______ for a few seconds.
  • Holding the RCL key down for more than _______ seconds will reactivate any _______ messages that were suppressed by the _____ _____ key.

VOL. II, 31.4.1.7

A

WRNG_02
Describe the purpose of the EMER CANC and RCL pbs.

  1. RCL
  • The RCL (recall) key allows the crew to call up warning messages, caution messages, and the status page that may have been suppressed by the activation of the CLR key or flight phase related inhibition.
  • If there are no suppressed warnings or cautions the E/WD displays NORMAL for a few seconds.
  • Holding the RCL key down for more than 3 seconds will reactivate any caution messages that were suppressed by the EMER CANC key.

VOL. II, 31.4.1.7

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9
Q

WRNG_03
Describe the purpose of TO CONFIG pb.
The T.O. CONFIG (takeoff configuration) key is used to _______ the application of takeoff power.

If the aircraft is not in the takeoff configuration when the T.O. CONFIG key is pushed or takeoff power is applied:

  • A takeoff configuration warning is displayed on the ______._
  • The _____ _____ lights flash.
  • The _______ sounds.

If the configuration is acceptable, the T.O. memo on the E/WD displays:

  • _____ _____ __________.

VOL II, 31.4.1.8

A

WRNG_03
Describe the purpose of TO CONFIG pb.
The T.O. CONFIG (takeoff configuration) key is used to simulate the application of takeoff power.

If the aircraft is not in the takeoff configuration when the T.O. CONFIG key is pushed or takeoff power is applied:

  • A takeoff configuration warning is displayed on the E/WD.
  • The MASTER WARN lights flash.
  • The CRC sounds.

If the configuration is acceptable, the T.O. memo on the E/WD displays:

  • T.O. CONFIG NORMAL.

VOL II, 31.4.1.8

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10
Q

WRNG_03
Describe the purpose of TO CONFIG pb.

Items checked using the T.O. CONFIG key include:

  • _____/_____ in takeoff range (config 1+F, 2, or 3)
  • _____ _____in takeoff range
  • ______ ______ in takeoff range
  • _____ _____s retracted
  • Sidestick _______ not engaged
  • ______s_ not hot
  • _______ closed (not checked with the engines shut down)

VOL II, 31.4.1.8

A

WRNG_03
Describe the purpose of TO CONFIG pb.

Items checked using the T.O. CONFIG key include:

  • Slats/flaps in takeoff range (config 1+F, 2, or 3)
  • Pitch trim in takeoff range
  • Rudder trim in takeoff range
  • Speed brakes retracted
  • Sidestick takeover not engaged
  • Brakes not hot
  • Doors closed (not checked with the engines shut down)

VOL II, 31.4.1.8

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11
Q

WRNG_03
Describe the purpose of TO CONFIG pb.

When takeoff power is applied two additional checks are performed:
_____ _____ released
• That a _______ temp setting has been entered on the PERF TAKE OFF page if thrust is set to ______._

VOL II, 31.4.1.8

A

WRNG_03
Describe the purpose of TO CONFIG pb.

When takeoff power is applied two additional checks are performed:
Parking brake released
• That a FLEX temp setting has been entered on the PERF TAKE OFF page if thrust is set to FLEX.

VOL II, 31.4.1.8

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12
Q

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.
Takeoff and Landing Memos
Memo checklists are automatically displayed for takeoff and landing.

  • The item names appear in _______ on each checklist.
  • Dot leaders and the action step appear in _______ if the action is _______ complete.
  • The dot leaders disappear and the action item changes to green when the_____ is completed.
  • When the checklist is complete the _____ _____ is displayed in green.

VOL. II, 31.4.2.4

A

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.
Takeoff and Landing Memos
Memo checklists are automatically displayed for takeoff and landing.

  • The item names appear in green on each checklist.
  • Dot leaders and the action step appear in blue if the action is not complete.
  • The dot leaders disappear and the action item changes to green when the step is completed.
  • When the checklist is complete the entire message is displayed in green.

VOL. II, 31.4.2.4

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13
Q

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.
Takeoff and Landing Memos

  • The T.O. (takeoff) memo appears [____] minutes after the _______ engine start
    • or when the __ _____ key on the ECAM control panel is pushed, provided at least one engine is running.
  • The message disappears at _______ power application.

The LDG (landing) memo appears when below [_______] feet AGL and disappears after _______

VOL. II, 31.4.2.4

A

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.
Takeoff and Landing Memos

  • The T.O. (takeoff) memo appears [2] minutes after the second engine start
    • or when the TO CONFIG key on the ECAM control panel is pushed, provided at least one engine is running.
  • The message disappears at takeoff power application.

The LDG (landing) memo appears when below [2000] feet AGL and disappears after touchdown.

VOL. II, 31.4.2.4

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14
Q

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.

Inhibit memos
Inhibit memos appear in _______ to indicate that, during the takeoff and landing phases of the flight, certain ___-____cautions are inhibited to prevent distracting the crew.

VOL. II, 31.4.2.3

A

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.

Inhibit memos
Inhibit memos appear in magenta to indicate that, during the takeoff and landing phases of the flight, certain non-critical cautions are inhibited to prevent distracting the crew.

VOL. II, 31.4.2.3

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15
Q

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.

Inhibit memos

The T.O. INHIBIT memo is displayed between application of _____ _____ and [_______] feet.

The LDG INHIBIT memo is displayed between [_______] feet and [______] knots.

These messages are only a reminder that should certain failures occur during these critical phases of flight, the associated _______ message will be inhibited. They do not indicate that a caution is ______y_ being inhibited.

If a failure occurred prior to the inhibition phase, the warning or caution indications ________ to be displayed and are not inhibited.

If the failure occurs during the inhibition phase, the indications are displayed as soon as the ________ no longer applies.

VOL. II, 31.4.2.3

A

WRNG_04
Recall the purpose of the checklists and inhibit memos on the E/WD.

Inhibit memos

The T.O. INHIBIT memo is displayed between application of takeoff power and [1500] feet.

The LDG INHIBIT memo is displayed between [800] feet and [80] knots.

These messages are only a reminder that should certain failures occur during these critical phases of flight, the associated caution message will be inhibited. They do not indicate that a caution is currently being inhibited.

If a failure occurred prior to the inhibition phase, the warning or caution indications continue to be displayed and are not inhibited.

If the failure occurs during the inhibition phase, the indications are displayed as soon as the inhibition no longer applies.

VOL. II, 31.4.2.3

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16
Q

WRNG_05
Recall what information can be found on the STATUS page.

Status Page

  • The status page can be accessed at any time and displays an _______ summary of the aircraft status.
  • Additionally, the STATUS page is the last page to auto-display following the completion of an ECAM _______ procedure.

Included on the status page are:

  • Limitations in _______
  • Corrections procedures to apply for landing in _______
  • Supplemental information in _______
  • _______ procedures in white, red or amber
  • _______ status
  • _______ systems
  • _______ cautions
  • _______ symbol

Status Reminder

  • If any messages exist on the STATUS page, the letters _______appear boxed at the base of the E/WD.

VOL. II, 31.4.3.7

A

WRNG_05
Recall what information can be found on the STATUS page.

Status Page

  • The status page can be accessed at any time and displays an operational summary of the aircraft status.
  • Additionally, the STATUS page is the last page to auto-display following the completion of an ECAM abnormal procedure.

Included on the status page are:

  • Limitations in blue
  • Corrections procedures to apply for landing in blue
  • Supplemental information in green
  • Approach procedures in white, red or amber
  • Maintenance status
  • Inoperative systems
  • Cancelled cautions
  • Overflow symbol

Status Reminder

  • If any messages exist on the STATUS page, the letters STS appear boxed at the base of the E/WD.

VOL. II, 31.4.3.7

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17
Q

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.
There are _______ types of failures:

  • _______ - A failure that affects an _______ system with no degrading performance on _______ aircraft systems or equipment.
  • _______ - A failure that results in the loss or degradation of _______ aircraft systems or equipment.
  • _______ - A failure or degradation resulting from a _______ failure.

VOL. II, 31.4.5.1

A

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.
There are three types of failures:

  • Independent - A failure that affects an isolated system with no degrading performance on other aircraft systems or equipment.
  • Primary - A failure that results in the loss or degradation of other aircraft systems or equipment.
  • Secondary - A failure or degradation resulting from a primary failure.

VOL. II, 31.4.5.1

18
Q

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

The lower portion of the E/WD is divided into _______ sections.

  • The left side of the display lists _____ and _____ failures, and any associated ______._
  • The right side of the display lists the _____ of _____ affected by other failures that cannot fit on the left side due to overflow.
  • The right side also lists _____ _____titles affected by primary failures and ______l_ messages such as LAND ASAP and AP OFF.

VOL. II, 31.4.5.1

A

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

The lower portion of the E/WD is divided into two sections.

  • The left side of the display lists independent and primary failures, and any associated checklists.
  • The right side of the display lists the title of systems affected by other failures that cannot fit on the left side due to overflow.
  • The right side also lists secondary system titles affected by primary failures and special messages such as LAND ASAP and AP OFF.

VOL. II, 31.4.5.1

19
Q

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

All failure messages are preceded by the affected system ____ ________

  • This section of the message corresponds to the appropriate _____ chapter. (e.g., HYD)
  • The next part of the message depicts the _______ of the failure and the corresponding _______ checklist reference.
    • (e.g., G+Y SYS LO PR)

VOL. II, 31.4.5.1

A

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

All failure messages are preceded by the affected system name underlined.

  • This section of the message corresponds to the appropriate QRH chapter. (e.g., HYD)
  • The next part of the message depicts the title of the failure and the corresponding QRH checklist reference.
    • (e.g., G+Y SYS LO PR)

VOL. II, 31.4.5.1

20
Q

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

  • A primary failure has a _____ title.
  • The other systems affected by that failure are depicted on the _____ side of the display, preceded by an ______._
  • _____ and _____ failures are not boxed.

VOL. II, 31.4.5.1

A

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

  • A primary failure has a boxed title.
  • The other systems affected by that failure are depicted on the right side of the display, preceded by an asterisk.
  • Independent and secondary failures are not boxed.

VOL. II, 31.4.5.1

21
Q

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

  • Action steps depicted below the title are in _______, and are to be completed by the pilot.
  • When an action step has been completed, the step usually ______._
  • Note: Action steps that cannot be monitored by the _______ (e.g., ATC NOTIFY), do not automatically clear from the E/WD

VOL. II, 31.4.5.1

A

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

  • Action steps depicted below the title are in blue, and are to be completed by the pilot.
  • When an action step has been completed, the step usually disappears.
  • Note: Action steps that cannot be monitored by the FWCs (e.g., ATC NOTIFY), do not automatically clear from the E/WD

VOL. II, 31.4.5.1

22
Q

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

A green _______ symbol is displayed at the base of the _______ when there is not enough room, on the left side of the display, to list all of the _____ or _____ failures.

Systems affected by i_____ or _____ failures that are not displayed on the left are shown on the _______ of the display (with __ _____).

As actions are performed, and higher priority abnormals are dealt with and cleared, room for the additional abnormals becomes available on the left.

The abnormals will automatically appear on the left side once there is room for them, and the overflow symbol will eventually disappear.
VOL. II, 31.4.5.1

A

WRNG_06
Describe the different type of ECAM warning/caution message indications on the E/WD.

A green overflow symbol is displayed at the base of the E/WD when there is not enough room, on the left side of the display, to list all of the independent or primary failures.

Systems affected by independent or primary failures that are not displayed on the left are shown on the right of the display (with no asterisk).

As actions are performed, and higher priority abnormals are dealt with and cleared, room for the additional abnormals becomes available on the left.

The abnormals will automatically appear on the left side once there is room for them, and the overflow symbol will eventually disappear.
VOL. II, 31.4.5.1

23
Q

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

  • The E/WD is normally depicted on the _______ DU,
  • and the SD is normally depicted on the _______ DU.
  • If only one DU is available, the _______ has priority over the ______._

VOL. II, 31.2.4.7

A

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

  • The E/WD is normally depicted on the upper DU,
  • and the SD is normally depicted on the lower DU.
  • If only one DU is available, the E/WD has priority over the SD.

VOL. II, 31.2.4.7

24
Q

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

If the upper DU fails or is turned OFF, the E/WD will:

  • automatically be displayed on the _______ DU.

If the lower DU fails or is turned OFF:

  • no _______ switching takes place, as the higher priority _______ is already displayed on the upper DU.

VOL. II, 31.2.4.7

A

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

If the upper DU fails or is turned OFF, the E/WD will:

  • automatically be displayed on the lower DU.

If the lower DU fails or is turned OFF:

  • no automatic switching takes place, as the higher priority E/WD is already displayed on the upper DU.

VOL. II, 31.2.4.7

25
Q

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

The SD can be regained by either:

  • Pushing and holding the desired system page pb on the _____ _____ _____.
    • In this case, the selected page will replace the _____ on the operable ECAM DU.
  • Selecting the _____/__ transfer switch to CAPT or FO.
    • In this case, the SD is transferred to the selected _______ DU (CAPT or FO),
    • and the _______ remains displayed on the upper DU.

VOL. II, 31.2.4.7

A

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

The SD can be regained by either:

  • Pushing and holding the desired system page pb on the ECAM control panel.
    • In this case, the selected page will replace the E/WD on the operable ECAM DU.
  • Selecting the ECAM/ND transfer switch to CAPT or FO.
    • In this case, the SD is transferred to the selected inner DU (CAPT or FO),
    • and the E/WD remains displayed on the upper DU.

VOL. II, 31.2.4.7

26
Q

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

If both ECAM DUs fail:

  • The E/WD can be displayed by selecting the ______/___ transfer switch to CAPT or F/O.
    • In this case, the E/WD is transferred to the selected _______ DU (CAPT or F/O).
  • The SD may be viewed on the inner DU by pushing and holding the _____ _____ _____ pb on the ECAM control panel.
    • In this case, the selected SD page will replace the _______ on the operable _____ DU for as long as the system page pb is held down.
A

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

If both ECAM DUs fail:

  • The E/WD can be displayed by selecting the ECAM/ND transfer switch to CAPT or F/O.
    • In this case, the E/WD is transferred to the selected inner DU (CAPT or F/O).
  • The SD may be viewed on the inner DU by pushing and holding the desired system page pb on the ECAM control panel.
    • In this case, the selected SD page will replace the E/WD on the operable inner DU for as long as the system page pb is held down.

VOL. II, 31.2.4.7

27
Q

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

If both ECAM DUs are operating normally, selecting CAPT or F/O will transfer the SD to the respective pilot’s _____ __.

VOL. II, 31.2.4.7

A

WRNG_07
Describe the ECAM display switching logic as well as the usage of the ECAM/ND selector.

If both ECAM DUs are operating normally, selecting CAPT or F/O will transfer the SD to the respective pilot’s inner DU.

VOL. II, 31.2.4.7

28
Q

WRNG_08
Understand the control functions and indications on the ECAM SWITCHING Selector.
ECAM SWITCHING Selector

  • Normally DMC 3 supplies data to the _______ ____s_.
  • The DMC selector on the ECAM SWITCHING panel allows the selection of _____, __, __, or __.

VOL. II, 31.2.4.8

A

WRNG_08
Understand the control functions and indications on the ECAM SWITCHING Selector.
ECAM SWITCHING Selector

  • Normally DMC 3 supplies data to the ECAM DUs.
  • The DMC selector on the ECAM SWITCHING panel allows the selection of AUTO, 1, 2, or 3.

VOL. II, 31.2.4.8

29
Q

WRNG_08
Understand the control functions and indications on the ECAM SWITCHING Selector.
ECAM SWITCHING Selector

In AUTO, DMC 3 normally supplies the ECAM DUs.

If the ECAM channel of DMC 3 fails, _______will:

  • automatically take over the ECAM display on the _____ DUs.

The DMC selector also allows for the _______ selection of any DMC’s ECAM channel (bypassing the automatic switching) by placing the switch in the 1, 2, or 3 position.

VOL. II, 31.2.4.8

A

WRNG_08
Understand the control functions and indications on the ECAM SWITCHING Selector.
ECAM SWITCHING Selector

In AUTO, DMC 3 normally supplies the ECAM DUs.

If the ECAM channel of DMC 3 fails, DMC 1 will:

  • automatically take over the ECAM display on the ECAM DUs.

The DMC selector also allows for the manual selection of any DMC’s ECAM channel (bypassing the automatic switching) by placing the switch in the 1, 2, or 3 position.

VOL. II, 31.2.4.8

30
Q

WRNG_09
Understand the control functions and indications on the GPWS panel.
The GPWS has _______ modes:

  • a _______ mode
  • and a _______ mode,
  • which are mostly _______ of each other.

Most failures affecting the _______ mode will not affect the _______ mode and vice versa.

However, the loss of certain inputs may cause both modes to fail.

Each mode can be controlled _______ using pbs located on the overhead GPWS panel.

VOL. II, 85.2.1.2

A

WRNG_09
Understand the control functions and indications on the GPWS panel.
The GPWS has two modes:

  • a basic mode
  • and a terrain mode,
  • which are mostly independent of each other.

Most failures affecting the basic mode will not affect the terrain mode and vice versa.

However, the loss of certain inputs may cause both modes to fail.

Each mode can be controlled independently using pbs located on the overhead GPWS panel.

VOL. II, 85.2.1.2

31
Q

WRNG_09
Understand the control functions and indications on the GPWS panel.

TERR Pb

  • Selected OFF - The terrain mode is _______
  • FAULT - A fault has occurred that affects the _______ mode.

VOL. II, 85.2.1.2

A

WRNG_09
Understand the control functions and indications on the GPWS panel.

TERR Pb

  • Selected OFF - The terrain mode is off.
  • FAULT - A fault has occurred that affects the terrain mode.

VOL. II, 85.2.1.2

32
Q

WRNG_09
Understand the control functions and indications on the GPWS panel.

SYS Pb

  • Selected OFF - The GPWS _______mode is off.
  • FAULT - A fault has occurred that affects the GPWS _______ mode.

VOL. II, 85.2.1.2

A

WRNG_09
Understand the control functions and indications on the GPWS panel.

SYS Pb

  • Selected OFF - The GPWS basic mode is off.
  • FAULT - A fault has occurred that affects the GPWS basic mode.

VOL. II, 85.2.1.2

33
Q

WRNG_09
Understand the control functions and indications on the GPWS panel.

G/S MODE Pb

  • Selected OFF - The “_____ _____” warning is inhibited.

VOL. II, 85.2.1.2

A

WRNG_09
Understand the control functions and indications on the GPWS panel.

G/S MODE Pb

  • Selected OFF - The “GLIDE SLOPE” warning is inhibited.

VOL. II, 85.2.1.2

34
Q

WRNG_09
Understand the control functions and indications on the GPWS panel.

FLAP MODE Pb

  • Selected OFF - The “_____ _____, _____” warning is inhibited.

VOL. II, 85.2.1.2

A

WRNG_09
Understand the control functions and indications on the GPWS panel.

FLAP MODE Pb

  • Selected OFF - The “TOO LOW, FLAPS” warning is inhibited.

VOL. II, 85.2.1.2

35
Q

WRNG_10
Recall what will occur on the ND when a terrain alert is generated.

  • The terrain display is automatically displayed on the NDs if a_____mode _____ _____ is generated.
  • If terrain is displayed on an ND, either automatically of manually, the terrain display inhibits the display of __________ _____ returns.

VOL. II, 85.2.3.7

A

WRNG_10
Recall what will occur on the ND when a terrain alert is generated.

  • The terrain display is automatically displayed on the NDs if a terrain mode terrain alert is generated.
  • If terrain is displayed on an ND, either automatically of manually, the terrain display inhibits the display of weather radar returns.

VOL. II, 85.2.3.7

36
Q

WRNG_11
Understand the control functions and indications on the ATC/TCAS panel as they relate to the TCAS system.
ATC/TCAS Panel

1. Mode Selector

  • STBY - TCAS is on _______.
  • TA - TCAS does not generate any _______ commands, only TAs are generated.
  • TA/RA - TCAS can generate _______l commands and all RAs, TAs, proximate, and other traffic can be displayed.

Note: Operation of TCAS in either TA/RA or TA mode requires that the _____ _____ switch is ON and the active transponder is selected to _____ or ___

VOL. II, 85.3.5

A

WRNG_11
Understand the control functions and indications on the ATC/TCAS panel as they relate to the TCAS system.
ATC/TCAS Panel

1. Mode Selector

  • STBY - TCAS is on standby.
  • TA - TCAS does not generate any vertical commands, only TAs are generated.
  • TA/RA - TCAS can generate vertical commands and all RAs, TAs, proximate, and other traffic can be displayed.

Note: Operation of TCAS in either TA/RA or TA mode requires that the ALT RPTG switch is ON and the active transponder is selected to AUTO or ON.

VOL. II, 85.3.5

37
Q

WRNG_11
Understand the control functions and indications on the ATC/TCAS panel as they relate to the TCAS system.
ATC/TCAS Panel

2. Traffic Selector

  • THRT (threat) - Other traffic and proximate traffic within [_____] feet are only displayed if a ___ or ___ is generated.
  • ALL - Other traffic and proximate traffic within [_____] feet are always displayed.
  • ABV (above) - Other traffic and proximate traffic from [_____] feet above to [_____] feet below are always displayed.
  • BLW (below) - Other traffic and proximate traffic from [_____] feet above to _____] feet below are always displayed.

VOL. II, 85.3.5

A

WRNG_11
Understand the control functions and indications on the ATC/TCAS panel as they relate to the TCAS system.
ATC/TCAS Panel

2. Traffic Selector

  • THRT (threat) - Other traffic and proximate traffic within [2700] feet are only displayed if a TA or RA is generated.
  • ALL - Other traffic and proximate traffic within [2700] feet are always displayed.
  • ABV (above) - Other traffic and proximate traffic from [9900] feet above to [2700] feet below are always displayed.
  • BLW (below) - Other traffic and proximate traffic from [2700] feet above to [9900] feet below are always displayed.

VOL. II, 85.3.5

38
Q

WRNG_12

Describe the different TCAS traffic types and their symbology on the ND.
The four types of traffic are:

  • Other - The aircraft is displayed but does not pose a _______ threat (maximum range of other aircraft for display: ____ NM)
  • Proximate - The aircraft does not currently pose a _______ threat but is within [____] NM.
  • Traffic Advisory (TA) - The intruder aircraft does not pose an _______ collision threat but is in _______ proximity to the aircraft.
    • An _______ warning to alert the crew to the close proximity of the intruder aircraft is annunciated.
  • Resolution Advisory (RA) - The intruder aircraft _______ an immediate collision threat.
    • An _______ warning commanding _______ evasive maneuvers to avoid collision with the intruder aircraft is annunciated (e.g., “CLIMB, CLIMB”).
    • A recommended _______ speed range is displayed on the PFDs.

VOL. II, 85.3.2.1

A

WRNG_12

Describe the different TCAS traffic types and their symbology on the ND.
The four types of traffic are:

  • Other - The aircraft is displayed but does not pose a collision threat (maximum range of other aircraft for display: 80 NM)
  • Proximate - The aircraft does not currently pose a collision threat but is within [6] NM.
  • Traffic Advisory (TA) - The intruder aircraft does not pose an immediate collision threat but is in close proximity to the aircraft.
    • An aural warning to alert the crew to the close proximity of the intruder aircraft is annunciated.
  • Resolution Advisory (RA) - The intruder aircraft poses an immediate collision threat.
    • An aural warning commanding vertical evasive maneuvers to avoid collision with the intruder aircraft is annunciated (e.g., “CLIMB, CLIMB”).
    • A recommended vertical speed range is displayed on the PFDs.

VOL. II, 85.3.2.1

39
Q

WRNG_12

Describe the different TCAS traffic types and their symbology on the ND.

Additionally, TCAS traffic displayed on the NDs:

  • Includes the relative _______ of the traffic and its _______ trend, if greater than [_______] feet per minute.
  • The location of the traffic on the NDs indicates its relative position.
  • The shape and color indicates the type of traffic and level of threat.
    • _______ - Hollow white diamond
    • _______ - Solid white diamond
    • _______ _____- Solid amber circle
    • _____ _____ - Solid red square

VOL. II, 85.3.2.1

A

WRNG_12

Describe the different TCAS traffic types and their symbology on the ND.

Additionally, TCAS traffic displayed on the NDs:

  • Includes the relative altitude of the traffic and its vertical trend, if greater than [500] feet per minute.
  • The location of the traffic on the NDs indicates its relative position.
  • The shape and color indicates the type of traffic and level of threat.
    • Other - Hollow white diamond
    • Proximate - Solid white diamond
    • Traffic Advisory - Solid amber circle
    • Resolution Advisory - Solid red square

VOL. II, 85.3.2.1

40
Q

THE END

A