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notches on the side of the head of the pushbutton
switch.
Carefully pull the tool to remove the heat of the
pusbutton switch.
The head stays attached to the body of the pushbutton
switch by the rods that turn.
Now you have to remote the body of the pushbutton
switch.
First, fully loosen the two screws of the body but do
not lock them.
After, pull the head to remote the body.
Before starting the installation of a pushbutton
switch, clean and make an inspection of the component
interface and of the adjacent area.
Now, put the TOP mark in the up position and push the
body of the pushbutton switch fully into its housing.
Torque the two screws of the body of the pushbutton
switch.
Now, install the head in the body of the pushbutton
switch.
To do this, push the head until it touches the stop.
To finish the installation task close the circuit
breaker of the circuit related to the pushbutton
switch.
After that, make sure that the work area is clean and
clear of tools and other items.
TMUGENE01-T01 LEVEL 1
EFFECTIVITY 31-00-00 Page 2
Oct 31/98
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 486
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31 - INDICATING/RECORDING SYSTEMS
31-00-00 CFDS SPECIFIC PAGE PRESENTATION
CONTENTS:
ECAM 1 General
ECAM 1 ECAM PIN PROGRAM
FDIU CREATE TEST
CFDIU
EIS 1 General
EIS 1 PREVIOUS LEGS REPORT
EIS 1 ENGINES
EIS 1 DUMP BITE MEMORY
EIS 1 TEST
TMUMCDU03 LEVEL 3
EFFECTIVITY 31-00-00 Page 1
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 487
ALL
CFDS SPECIFIC PAGE PRESENTATION
ECAM 1 GENERAL
ECAM 1 corresponds to FWC1, SDAC1 and ECP.
ECAM 2 corresponds to FWC2, SDAC2 and ECP.
ECAM 1 ECAM PIN PROGRAM
The first page of ECAM PIN PROGRAM gives the status
of SDAC1 and SDAC2 hardware pin programming.
The second page gives the status of FWC1 and FWC2
hardware pin programming.
TMUMCDU03-T01 LEVEL 3
EFFECTIVITY 31-00-00 Page 2
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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ALL
CFDS SPECIFIC PAGE PRESENTATION - ECAM 1 GENERAL/ECAM PIN PROGRAM
TMUMCDU03-P01 LEVEL 3
EFFECTIVITY 31-00-00 Page 3
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 489
ALL
CFDS SPECIFIC PAGE PRESENTATION
FDIU CREATE TEST
CREATE TEST activates the test immediately and displays
the result.
TMUMCDU03-T02 LEVEL 3
EFFECTIVITY 31-00-00 Page 4
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
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CFDS SPECIFIC PAGE PRESENTATION - FDIU CREATE TEST
TMUMCDU03-P02 LEVEL 3
EFFECTIVITY 31-00-00 Page 5
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 491
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CFDS SPECIFIC PAGE PRESENTATION
CFDIU
No specific functions (Refer to ATA chapter 31 "CFDS
Reports" module).
NOTE: CFDIU is a type 1 system but there is no PREVIOUS
LEGS REPORT.
TMUMCDU03-T03 LEVEL 3
EFFECTIVITY 31-00-00 Page 6
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 492
ALL
CFDS SPECIFIC PAGE PRESENTATION - CFDIU
TMUMCDU03-P03 LEVEL 3
EFFECTIVITY 31-00-00 Page 7
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 493
ALL
CFDS SPECIFIC PAGE PRESENTATION
EIS 1 GENERAL
As long as DMC1 is in maintenance mode, the CAPT PFD
and ND and the upper ECAM Display Units will display
"MAINTENANCE MODE" instead of the regular operational
mode.
EIS 1 PREVIOUS LEGS REPORT
Error codes are used in some DMC identification
messages. They give a more precise failure
identification. When required, the trouble shooting
manual will help you to identify the code.
In this example, "1001" is the error code. (3) means
　
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