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EFFECTIVITY 31-36-00 Page 19
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
ENGINE RUN UP REPORT <11>
This report is primarily generated on manual request.
It contains the same data as the ENGINE CRUISE REPORT
<01> plus corrected parameters for the ambient
temperature.
These corrected data are averages over a period of 20
seconds as well as most of the other report data (refer
to the ENGINE CRUISE REPORT <01> topic).
TMUAI2G02-T10 LEVEL 3
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION - ENGINE RUN UP REPORT <11>
TMUAI2G02-P10 LEVEL 3
EFFECTIVITY 31-36-00 Page 21
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
APU MAIN ENGINE START/IDLE REPORT <13>
This report is generated once at the beginning of each
new APU operating hour interval when a main engine is
started with the APU.
The APU operating hour interval is programmable.
The report mainly contains operating data of the APU:
- from each Main Engine Start (MES) (lines N1,
S1 and N2, S2).
If the APU master switch is set to off before
the second MES is terminated, lines N2 and S2
are filled with zeros.
- at APU idle (lines N3 and S3).
In addition, line V1 contains data from the previous
APU start.
TMUAI2G02-T11 LEVEL 3
EFFECTIVITY 31-36-00 Page 22
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION - APU MAIN ENGINE START/IDLE REPORT <13>
TMUAI2G02-P11 LEVEL 3
EFFECTIVITY 31-36-00 Page 23
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
APU SHUTDOWN REPORT <14>
This report is generated in case of abnormal APU
shutdown.
The possible shutdown reasons are:
- no flame,
- reverse flow,
- loss of DC power,
- high oil temperature,
- air intake not open,
- generator high oil temperature,
- overtemperature,
- sensor failure,
- no acceleration,
- start time exceeded,
- overspeed,
- ECB failure,
- low oil pressure,
- loss of speed,
- IGV failure.
When effective, the reason is displayed.
Basically, 20 sets of APU parameters are recorded at
1 second intervals before the event and 1 set at the
event.
The length of the pre-event interval (Y14.1) is
programmable.
TMUAI2G02-T12 LEVEL 3
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION - APU SHUTDOWN REPORT <14>
TMUAI2G02-P12 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
LOAD REPORT <15>
Basically, this report is generated when excessive
loads are applied to the airframe during landing.
The report mainly contains aircraft aerodynamic data
recorded before, at and after a hard landing.
An aircraft bounce can also be detected.
In that case, additional data lines T1 to T4 are also
generated.
TMUAI2G02-T13 LEVEL 3
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MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION - LOAD REPORT <15>
TMUAI2G02-P13 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
　
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