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the DMU.
NOTES: - In this module, reports <01> to <11> are given
for a CFM engine. They may be slightly different
to your aircraft configuration.
- Depending on the DMU which is fitted on your
aircraft, the LOAD REPORT <15> may not be
applicable.
TMUAI2G02-T01 LEVEL 3
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION - GENERAL
TMUAI2G02-P01 LEVEL 3
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
ENGINE CRUISE REPORT <01>
This report is a collection of data over a period of
time in which the aircraft met the appropriate
stability criteria.
The required stability period is 100 seconds
(programmable value).
Basically, whatever the number of times the stability
is detected, only one report is generated per flight
leg. This report contains the data with the best engine
quality number (QE) over the whole flight leg.
If no stability is detected, then a report is generated
with the following message in its last line: "NO STABLE
FRAME CONDITION".
NOTE: In case the ENGINE DIVERGENCE REPORT <09> is
generated, an engine cruise report is also
generated when the first stability is detected,
regardless of quality.
The report mainly contains operating data of both
engines, including vibration data.
The report data are averages over the required
stability period, except:
- ESN, EHRS, ERT, ECYC: Engine general data
(serial number, flight hours, running time,
cycle).
- AP: Autopilot status.
- QE: Engine quality number used as stability
indicator for this report (00: best stability,
99: worst stability).
- OIQH: Oil consumption from the previous flight.
- EVM, ECW1, SSEL: Engine vibration status word,
engine control word, status of Full Authority
Digital Engine Control (FADEC) sensors.
- Data lines V3, V4: Averaged values taken from
the last stable descent (i.e. descent of the
last leg).
- Data lines V5, V6: Averaged values taken from
the last stable climb (i.e. climb of the current
leg).
NOTE: For engine health monitoring purposes, 3
additional sensors can be optionally connected
to the FADEC to permit recording of the following
parameters: PS13 (fan tip discharge pressure),
P25 (HP compressor inlet pressure), T5 (LP
turbine discharge temperature).
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION - ENGINE CRUISE REPORT <01>
TMUAI2G02-P02 LEVEL 3
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AIDS: INDIVIDUAL PRINT REPORT DESCRIPTION
CRUISE PERFORMANCE REPORT <02>
This report is similar to ENGINE CRUISE REPORT <01>
except that more information is provided about the
aircraft.
The following data is added:
- QA: Aircraft quality number used as stability
indicator for this report (00: best stability,
99: worst stability).
- WFQ: Inner cell fuel quantity.
- ELEV: Elevator position.
- AOA, SLP: Corrected angle of attack and side
slip angle.
- CFPG, CIVV: Last DMU calculated flight path
acceleration and inertial vertical speed.
- ROLL, YAW: Roll angle and body axis yaw rate
(average).
- THDG, LONP, LATP: True heading, longitude and
latitude positions.
- WS, WD: Wind speed and direction (average).
- FT, FD: Fuel temperature and density (average).
- Flight controls positions (average). E.g. RSP5:
Roll spoiler 5 position.
NOTE: Data lines X1, X4, X6 are issued from system 1
(e.g. FLAP system 1) or left (e.g. left spoiler
5) while data lines X2, X5, X7 are issued from
system 2 or right.
In addition, the trigger logic for this report differs
a little bit from the logic for ENGINE CRUISE REPORT
<01> and is performed independently (e.g. the required
stability period can be different).
TMUAI2G02-T03 LEVEL 3
　
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