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EFFECTIVITY 31-36-00 Page 6
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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 - CRUISE PERFORMANCE REPORT <02>
TMUAI2G02-P03 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
ENGINE TAKE OFF REPORT <04>
This report is generated while in the take off flight
phase when the sum of the Exhaust Gas Temperature (EGT)
for both engines is maximum. It is used to check the
trend and the stress of the engines during take off.
Basically, one report is generated per leg
(programmable frequency).
The report mainly contains data of both engines,
including the maximum EGT (EGTM).
The radio height (RALT), provided by radio altimeters
1 and 2, is also printed.
"T/O DELTA N1 SUMMARY" DATA
History of the difference between the maximum value
of N1 (N1MX) and the actual N1 during previous take
offs is provided for both engines.
"T/O DELTA N1 SUMMARY" data is calculated a few seconds
after entry into the take off flight phase,
independently from the report trigger.
TMUAI2G02-T04 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 TAKE OFF REPORT <04>
TMUAI2G02-P04 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
ENGINE REPORT ON REQUEST <05>
This report is a time series collection of engine
parameters and is only generated on manual request.
Parameters for both engines are recorded at 1 second
intervals, from 5 seconds before the request to 5
seconds after.
TMUAI2G02-T05 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 REPORT ON REQUEST <05>
TMUAI2G02-P05 LEVEL 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 449
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
ENGINE GAS PATH ADVISORY REPORT <06>
This report is generated by any of the following
trigger conditions:
- Stall condition detected on one engine.
- Exceedance of one of the primary engine
parameters (EGT, N1, N2) detected on one
engine.
- Fuel shut off valve closed in flight for at
least 4 seconds on one engine.
The reason for exceedance is displayed (STALL, EGT,
N1, N2, SHUT DOWN).
Basically, 3 sets of parameters for both engines are
recorded at 6 seconds intervals before the event, 1
set at the event and 5 sets at 5 seconds intervals
after the event.
The length of the pre-event and post-event intervals
(Y1 and Y2) is programmable.
The number of datasets to be generated after the event
is also programmable (up to 20). Report generation
stops when this number is reached or when the
exceedance parameters are again within their limit.
LIMIT EXCEEDANCE SUMMARY
The following data provides a summary on the exceedance
that occurred:
- E: Engine (1 or 2) on which the exceedance
occurred.
- MAX: Maximum value (peak) of the exceeded
parameter.
- LIM: Programmable limit that was exceeded.
- REF: N2 at stall detection (for all other
exceedance, zeros are printed).
- TOL: Time over limit during report generation.
- TTP: Time to peak during report generation.
TMUAI2G02-T06 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 - ENGINE GAS PATH ADVISORY REPORT <06>
TMUAI2G02-P06 LEVEL 3
EFFECTIVITY 31-36-00 Page 13
　
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