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时间:2011-04-29 11:48来源:蓝天飞行翻译 作者:航空
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FDEs and their correlated maintenance message summary groups show in time order of occurrence, with the most recent FDE and correlated maintenance message summary groups at the top of the list. The non-FDE summary groups show at the bottom of the list.
The present leg faults display also shows maintenance message summary groups for a single ATA chapter, which the CMCF stores in fault history leg 0.
The present leg faults display shows:
*
Header Information

*
Instructions field

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Fault summary field title

*
Number of items

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Fault summary field

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Buttons.


Header Information
The data under the main menu bar on the right side shows:
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Tail identification

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Flight number from the FMCF

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Leg ID, departure airport and arrival airport identifiers from the FMCF

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Leg start time and date from the CMCF

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CMCF source field.


Fault Summary Field Title
The fault summary field title shows above the fault summary field on the left side. The fault summary title shows:
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Data Recorded During the Present Leg -shows when the present leg faults display shows FDE and non-FDE summary groups

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Maintenance Messages Recorded During the Present Leg for XXXXX; (XXXXX is the ATA system that has faults) -shows when the present leg faults display shows maintenance message summary groups sorted by a single ATA chapter.


Number of Items
The number of items shows above the fault summary field on the right side. The number in the parentheses shows the total number of:

EFFECTIVITY BEJ ALL  45-10-00 
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CMCS -PRESENT LEG FAULTS DISPLAY

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FDE summary groups plus one for the non-FDE summary group, when the fault summary field shows FDE and non-FDE summary groups

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Maintenance message summary groups, when the fault summary field shows maintenance message summary groups for a single ATA chapter.


Fault Summary Field
A fault summary field has:

*
FDE summary groups

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Non-FDE summary group


*
Maintenance message summary groups for a single ATA chapter.


The summary groups are faults and FDEs which the CMCF stores in the current leg. The fault summary field border highlights when the cursor is within the area of the fault summary field and there is one or more summary groups within the field.
Select the cursor control device button while the cursor is within the area of the fault summary field to highlight the text of a maintenance message summary group or the text of a FDE summary group header. Select a button to show more data for the highlighted maintenance message summary group or the highlighted FDE summary group header.
FDE Summary Group
A FDE summary group shows the:
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Flight deck effect EICAS message and level

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Flight deck effect activity

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Fault code for the FDE

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Time and date the FDE occurred

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One or more maintenance message summary groups.


FDE and Maintenance Message Activity
The activity of an FDE shows as one of these:
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Active

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Latched

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Not Active.


An active FDE is an FDE that currently shows in the flight deck.
A latched FDE can only be a status message or a scheduled maintenance task. Scheduled maintenance tasks are discussed in other parts of this section.
A failure that caused a status message may impact dispatch and may be intermittent or detectable only under certain conditions. The PDS holds a status message to make sure you can see it on the ground. You must do something to clear a latched FDE.
An FDE is not active if it can not currently be seen on the flight deck.

EFFECTIVITY BEJ ALL  45-10-00 
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D633W101-BEJ  Sep 05/2002 

 

CMCS -PRESENT LEG FAULTS DISPLAY

The activity of a maintenance message also shows as one of these:
*
Active

*
Latched

*
Not Active.

 

A maintenance message is active if a system can continuously monitor for a fault condition, and the fault exists.
A maintenance message is latched for one of these reasons:

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If a system detected a fault and is no longer using the related equipment as part of its operational function

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To ensure correlation with an FDE

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If a system can not always detect if the fault exists.

 

You must do something to clear a latched maintenance message.
A maintenance message is not active if a system can continuously monitor for a fault condition, and the fault does not exist.
 
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