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Air Data / Inertial Reference Units.
CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)
The Cabin Intercommunication Data System receives slat
flap position discretes for automatic lighting of cabin
passenger signs.
ENGINE INTERFACE UNITS (EIUs)
The Engine Interface Unit receives a slat flap lever
retracted position discrete for minimum idle.
Slat channel interface is identical.
TMUFCTE02-T02 LEVEL 3
EFFECTIVITY 27-00-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
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SFCC MONITOR INTERFACES
TMUFCTE02-P02 LEVEL 3
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUFCTE02 LEVEL 3
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27 - FLIGHT CONTROLS
27-00-00 CFDS SPECIFIC PAGE PRESENTATION
CONTENTS:
EFCS 1 (Specific Pages)
SFCC-1 (Specific Pages)
TMUFCPG05 LEVEL 3
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CFDS SPECIFIC PAGE PRESENTATION
EFCS 1
LAST LEG REPORT
The LAST LEG REPORT displays all the system failures
which appeared during the last flight.
The failure messages contain the name of the failed
LRU associated with the time at which the failure
occured and the ATA reference.
TROUBLE SHOOTING DATA
The TROUBLE SHOOTING DATA displays complementary fault
information concerning the system status before and
after the failure occurence.
This function can be called from the "LAST LEG REPORT"
and "PREVIOUS LEGS REPORT".
EFCS 1
PREVIOUS LEGS REPORT
The PREVIOUS LEGS REPORT presents failure messages
having affected the system during the previous 64
flight legs.
The additional information presented is identical to
that presented in the LAST LEG REPORT.
EFCS 1
MEMORY
The bite memory is used for workshop maintenance only.
It gives information in hexadecimal code.
TMUFCPG05-T01 LEVEL 3
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CFDS SPECIFIC PAGE PRESENTATION
TMUFCPG05-P01 LEVEL 3
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CFDS SPECIFIC PAGE PRESENTATION
EFCS 1
TEST
CAUTION : SURFACES WILL MOVE
AILERON DAMPING TEST
This test is driven by the FCDC and performed by the
two ELACs.
For each movement the FCDC memorizes a deflection speed
and a pressure drop, then it deducts a damp factor.
The test is not satisfactory when one of the four damp
factors is lower than the minimum value.
Tested components : aileron servo control actuators
TMUFCPG05-T02 LEVEL 3
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CFDS SPECIFIC PAGE PRESENTATION
TMUFCPG05-P02 LEVEL 3
EFFECTIVITY 27-00-00 Page 5
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CFDS SPECIFIC PAGE PRESENTATION
SFCC-1
Normally two SFCC menu pages are transmitted to the
CFDS by the selected SFCC.
But, in case of:
- PIN PROGRAMMING DISAGREEMENT
If there is a Pin Programming disagreement
installation, the SFCC transmits a " PIN PROG
DISAGREE " message.
In this case, no further pages shall be
provided.
- SLAT CHANNEL NOT AVAILBLE
If slat channel is selected but not available
the SFCC transmits a " SLAT NOT AVAILABLE "
message in all options.
SLT SYSTEM STATUS
The display features the faults (class 1 or 2)
affecting the system at the time of interrogation.
TMUFCPG05-T03 LEVEL 3
EFFECTIVITY 27-00-00 Page 6
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