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时间:2010-05-01 10:09来源:蓝天飞行翻译 作者:admin
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and Detection System (FIDS) presents the content of
the memories of this BITE starting by the most recent
fault.
This content gives a CFDS level 3 information
(engineering maintenance).
If other faults exist, they are accessible by pushing
the NEXT PAGE key on the MCDU.
TMUAFPG02-T02 LEVEL 3
EFFECTIVITY 22-00-00 Page 4
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 288
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CFDS SPECIFIC PAGE PRESENTATION
TMUAFPG02-P02 LEVEL 3
EFFECTIVITY 22-00-00 Page 5
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 289
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CFDS SPECIFIC PAGE PRESENTATION
GROUND SCAN
GROUND REPORT
The GROUND REPORT function enables the failures
recorded in the ground area of the FIDS memory to be
displayed.
Two types of content can be displayed:
- Normally, only the internal failures that
occured on ground.
- Or all internal and external failures found
after selection of the PRESENT FAILURES SCAN
function.
The content of this ground area is also erased during
computer power up and engine start.
NOTE:
- The ground area of the FIDS memory has the
capacity to store the 3 most recent failures,
the others being eliminated.
- The option and the information displayed are
similar to the LAST LEG REPORT.
PRESENT FAILURE SCAN
The philosophy of the PRESENT FAILURE SCAN function
is the same as the one describe about GROUND SCANNING
in ATA chapter 31 ("CFDS reports"), but results are
presented in a different way (same as LAST LEG REPORT
page).
The scan runs during 40 seconds, then the messages are
displayed on the GROUND REPORT page. A maximum of three
failures, internal or external, present at that time
can be displayed.
Each processor (example : FMGC1 COM) can announce one
failure only (the failure with the highest priority).
If 2 failures are present at same time No1 has to be
solved first in order to announce No2 in a second
PRESENT FAILURES SCAN report.
NOTE: The PRESENT FAILURE SCAN function erases the
ground contexts previously recorded, so it is
highly recommended to display it by using first
the GROUND REPORT function.
PROGRAM
The three report options are not available for the
operators. Only the manufacturer can use them through
an access code for development purposes.
The AFS/PROGRAM page is independent from the ground
scan function.
TMUAFPG02-T03 LEVEL 3
EFFECTIVITY 22-00-00 Page 6
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 290
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUAFPG02-P03 LEVEL 3
EFFECTIVITY 22-00-00 Page 7
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 291
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CFDS SPECIFIC PAGE PRESENTATION
WINDSHEAR TEST
This test checks that the system transmits and
presents:
- Visual and aural indications of the WINDSHEAR
warning (red WINDSHEAR legend displayed on PFDs
and WINDSHEAR three times announcement
generated by the FWC).
- Messages to indicate the loss of the
function (WINDSHEAR DET FAULT on the upper
ECAM display).
TMUAFPG02-T04 LEVEL 3
EFFECTIVITY 22-00-00 Page 8
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 292
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUAFPG02-P04 LEVEL 3
EFFECTIVITY 22-00-00 Page 9
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 293
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TMUAFPG02 LEVEL 3
EFFECTIVITY 22-00-00 Page 10
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 294
ALL


 
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