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- PH: DMU flight phase (based on flight phase
from FWC),
- CNT: Counter of the reports previously
generated (first 3 digits) and previous report
number (last 2 digits),
- CODE: Trigger condition code,
- BLEED STATUS,
- APU: APU bleed valve state,
- TAT: Total air temperature,
- ALT: Standard altitude,
- CAS: Computed air speed,
- MN: Mach number,
- GW: Gross weight,
- CG: Center of gravity,
- DMU/SW: DMU software partnumber.
TRIGGER CONDITION CODE
To identify the trigger condition that caused the
generation of a report, a numerical code is provided:
- 1000: Manual selection via MCDU,
- 2000: Flight phase dependent manual selection
via AIDS PRINT pushbutton when programmed by
the airline,
- 3000: Start logic programmed by the airline,
- 4000 to 7000: Report triggered by a combination
of logic conditions (refer to AMM 31-36-00 for
the detailed trigger logics associated to each
report),
- 8100 and 8200: Air Traffic Service Unit (ATSU)
uplink request.
BLEED STATUS
Bleed status is indicated with discrete coded
information and numerical values.
In the discrete coded information, 0 indicates that
the valve is closed and 1 indicates that the valve is
open.
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AIDS: PRINT REPORT STANDARD HEADER DESCRIPTION - GENERAL DATA
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SELF EXAMINATION
How are the standard headers?
A - Specific for each report.
B - Similar for all the reports.
C - Similar only for the engine reports.
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31 - INDICATING/RECORDING SYSTEMS
31-36-00 AIDS: INDIVIDUAL PRINT REPORT
DESCRIPTION
CONTENTS:
GENERAL
ENGINE CRUISE REPORT <01>
CRUISE PERFORMANCE REPORT <02>
ENGINE TAKE OFF REPORT <04>
ENGINE REPORT ON REQUEST <05>
ENGINE GAS PATH ADVISORY REPORT <06>
ENGINE MECHANICAL ADVISORY REPORT <07>
ENGINE DIVERGENCE REPORT <09>
ENGINE START REPORT <10>
ENGINE RUN UP REPORT <11>
APU MAIN ENGINE START/IDLE REPORT <13>
APU SHUTDOWN REPORT <14>
LOAD REPORT <15>
ENVIRONMENTAL CONTROL SYSTEM REPORT <19>
SELF EXAMINATION
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
GENERAL
A report is a comprehensive set of data related to a
specific event (e.g. limit exceedance of engine
parameters).
The parameters contained in the reports are among the
parameters provided with an alpha call-up (refer to
AMM 31-36-00 for the detailed parameter list associated
to each report).
The Data Management Unit (DMU) processes up to 23
different types of report:
- 13 standard reports for basic aircraft, engine
and APU monitoring.
These reports have fixed trigger mechanism,
fixed data collection and fixed output
formatting.
Nevertheless, certain constants and limits
within fixed trigger logics are reprogrammable.
Specific trigger conditions can be created for
each report by means of the Ground Support
Equipment (GSE).
- Up to 10 additional reports, numbered from 31
to 40, for airline specific investigation and
trouble shooting.
These reports are user programmable with the
GSE for trigger conditions, data collection,
report format and output destination.
In addition to the automatic trigger logics, all the
reports can be manually generated:
- via MCDU,
- via AIDS PRINT pushbutton (according to flight
phase associations, if programmed),
- via Air Traffic Service Unit (ATSU) (uplink
request).
Refer to AMM 31-36-00 for the detailed trigger logics
associated to each report.
A non-volatile memory for storage of at least 10
reports per different type of report is provided within
　
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