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AUTO FLIGHT SYSTEM COMPONENTS - MULTIPURPOSE CONTROL AND DISPLAY UNITS (MCDUs)
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AUTO FLIGHT SYSTEM COMPONENTS
FAC PUSHBUTTON SWITCHES
IDENTIFICATION
FIN: 12CC1, 12CC2
LOCATION
ZONE:
23VU (12CC1), 24VU (12CC2)
COMPONENT DESCRIPTION
The FAC pushbutton switch monitors the status of the
computer in a general way.
The FAULT indication comes on when a failure occurs
affecting the normal operation of the different FAC
functions.
The FAC pushbutton switch, when used, either disables
the related FAC operations (OFF light on - pressed
out) or enables the reset of the computer if pressed
in again (OFF light off).
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AUTO FLIGHT SYSTEM COMPONENTS - FAC PUSHBUTTON SWITCHES
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22 - AUTO FLIGHT SYSTEM
22-00-00 CFDS SPECIFIC PAGE PRESENTATION
CONTENT:
Nota
Last Leg Report
Previous Legs Report
Trouble Shooting Data
Ground Scan
Windshear Test
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CFDS SPECIFIC PAGE PRESENTATION
NOTA
- LRU ident is not a specific option.Refer to
ATA chapter 31 ("CFDS Reports").
- AFS TEST and LAND TEST functions are
respectively described in dedicated modules
("Operational test of the AFS and Operational
test of the LAND CAT III capability").
LAST LEG REPORT
The philosophy of the LAST LEG REPORT is the same as
the one described in ATA chapter 31 ("CFDS REPORT"),
but additional information is presented:
- FAIL NO : Number of presented fault. This
counter is reset at the start of each flight.
- OCCURENCE : Number of times the same failure
occurs within the same flight.
- ISSUED BY : Designates the computer which
detected the fault. By selecting this function
you have access to the primary data of the
analysis (TROUBLE SHOOTING DATA page).The
information presented on this page is the same
as that accessible by selecting the TROUBLE
SHOOTING DATA function from the AFS MAIN MENU
page.
NOTE: The last fault presented occured first during
the last flight (FAIL NO 01).
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CFDS SPECIFIC PAGE PRESENTATION
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CFDS SPECIFIC PAGE PRESENTATION
PREVIOUS LEGS REPORT
The philosophy of the PREVIOUS LEGS REPORT is the same
as the one described in ATA chapter 31 ("CFDS REPORT"),
and additional information presented is identical to
that presented in the LAST LEG REPORT.
TROUBLE SHOOTING DATA
From the AFS/TROUBLE SHOOTING BITE SELECTION page
generated by the Fault Isolation and Detection System
(FIDS) you can select the BITE that you wish to examine.
NOTE:
- FAC: Flight Augmentation Computer.
- FG: Flight Guidance.
- FM: Flight Management.
- COM: Command side.
- MON: Monitor side.
When the BITE has been selected, the Fault Isolation
　
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