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the DMU to a ground station via radio transmission.
The download of reports can be automatically initiated
by the DMU or manually initiated from the MCDU.
The ATSU can also receive from the ground, and send
to the DMU, requests for report generation and
reprogramming messages.
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SELF EXAMINATION
Which are the main functions of the AIDS?
A - Recording of the mandatory flight data
requested by the airworthiness authority.
B - Trouble shooting of avionics computers
only.
C - Engine condition, APU condition and
aircraft performance monitoring.
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31 - INDICATING/RECORDING SYSTEMS
31-36-00 AIDS: AIDS BASIC OPERATION
CONTENTS:
Real Time Parameter Read Out
Report Control
SAR Control
DAR Control
Self Examination
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AIDS: AIDS BASIC OPERATION
REAL TIME PARAMETER READ OUT
Parameters delivered to the Data Management Unit (DMU)
by aircraft systems can be called up in real time on
the Multipurpose Control and Display Unit by selecting
one of the two following functions:
- Parameter label call-up.
- Parameter alpha call-up.
PARAMETER LABEL CALL-UP
The parameter label call-up function enables the
display of parameters by using ARINC 429
characteristics.
Parameters are displayed in raw values and refreshed
once per second.
Up to 16 parameters can be simultaneously monitored
(8 pages with 2 parameters per page).
PARAMETER ALPHA CALL-UP
The parameter alpha call-up function enables the
display of parameters by using the corresponding
alphanumeric code (if defined).
E.g. RSP3 is the alphanumeric code to call up the left
and right Roll Spoiler 3 Position parameters.
Parameters are displayed in engineering values and
refreshed once per second.
Up to 20 alpha call-ups, with one or 2 parameters, can
be simultaneously displayed (5 pages with 4 alpha
call-ups per page).
NOTE: A predefined list of alpha call-ups is initially
provided within the DMU customer database.
Additional alpha call-ups can be defined with
the optional Ground Support Equipment (GSE).
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AIDS: AIDS BASIC OPERATION - REAL TIME PARAMETER READ OUT
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AIDS: AIDS BASIC OPERATION
REPORT CONTROL
A report consists of a fixed and comprehensive set of
data collected under predefined trigger logics.
There are 13 standard reports for basic aircraft,
engine and APU monitoring. Up to 10 additional reports
can be entirely defined by the user with the GSE.
Beside the automatic trigger logics (e.g. limit
exceedance of engine parameters), all the reports can
be manually generated via the MCDU, the AIDS PRINT
pushbutton or the Air Traffic Service Unit (ATSU).
The automatically or manually generated reports are
stored in a non-volatile memory of the DMU.
If programmed with the GSE, the reports can be
automatically stored in an optional PCMCIA disk in
parallel with the normal storage in the DMU.
Finally, the reports can be:
- automatically printed out or downlinked, via
ATSU (according to generation request and GSE
programming),
- manually printed out or downlinked, via ATSU
(upon MCDU request),
- automatically dumped on a Portable Data
Loader (PDL) floppy disk or a Personal
Computer Memory Card Association (PCMCIA)
disk (at "automatic dump disk" insertion).
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