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IDENTIFICATION
FIN: 13 HC, 14 HC
LOCATION
ZONE: 154, 160
COMPONENT DESCRIPTION
used for temperature control, indication and overheat
detection.
TMUVENP0A-T07 LEVEL 3
EFFECTIVITY 21-28-00 Page 14
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 316
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TMUVENP0A-P07 LEVEL 3
AFT CARGO COMPARTMENT VENTILATION/HEATING - COMPONENTS - TEMPERATURE SENSORS
EFFECTIVITY 21-28-00 Page 15
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 317
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TMUVENP0A LEVEL 3
EFFECTIVITY 21-28-00 Page 16
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 318
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21 - AIR CONDITIONING
21-00-00 CFDS SPECIFIC PAGE PRESENTATION
CONTENTS:
CPC 1
Last Leg Report
Previous Legs Report
Class 3 Faults
TEMP CTL
Last Leg Report
Previous Legs Report
GND Report
FWD CHC & AFT CHC
Last Leg Class 3 Faults
Ground Report
TMUTEMY01 LEVEL 3
EFFECTIVITY 21-00-00 Page 1
Nov 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 319
ALL
CFDS SPECIFIC PAGE PRESENTATION
CPC 1
LAST LEG REPORT
This item presents the same type of failure messages
as described in chapter 31 (type 1 system) with the
same presentation, the FIN number is in addition.
NOTE: a GND indication appears at the end of the failure
messages in case of failure detected on the
ground.Fault codes are transmitted in addition
to CFDS messages (engineering level).
PREVIOUS LEGS REPORT
This item presents the same type of failure messages
as described in chapter 31 (type 1 system) with
different presentation: phase, FIN and flight number
indications are added to the leg, the date, time and
ATA reference indications.
NOTE: a GND indication appears at the end of the failure
messages in case of failure detected on the
ground.
Fault codes are transmitted in addition to CFDS
messages (engineering level).
CLASS 3 FAULTS
This item presents the same type of failure messages
as described in chapter 31 (type 1 system) with
different presentation: leg, phase and FIN number
indications are added to the date, time and ATA
reference indications.
Fault codes are transmitted in addition to CFDS
messages (engineering level).
TMUTEMY01-T01 LEVEL 3
EFFECTIVITY 21-00-00 Page 2
Nov 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 320
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUTEMY01-P01 LEVEL 3
EFFECTIVITY 21-00-00 Page 3
Nov 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 321
ALL
CFDS SPECIFIC PAGE PRESENTATION
TEMP CTL
LAST LEG REPORT
This item presents the same type of failure messages
as described in chapter 31 (type 1 system) with the
same presentation, the FIN number is in addition.
PREVIOUS LEGS REPORT
This item presents the same type of failure messages
as described in chapter 31 (type 1 system) with
different presentation: phase and FIN number
indications are added to the leg, the date, time and
ATA reference indications.
GND REPORT
This item is the equivalent of the LAST LEG REPORT for
the failures that have occured on the ground.
The failure messages contain the time, the phase, the
ATA reference and the FIN number.
TMUTEMY01-T02 LEVEL 3
EFFECTIVITY 21-00-00 Page 4
Nov 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 322
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUTEMY01-P02 LEVEL 3
EFFECTIVITY 21-00-00 Page 5
Nov 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 21 AIR CONDITIONING
UF94200
EFFECTIVITY Page 323
ALL
CFDS SPECIFIC PAGE PRESENTATION
FWD CHC & AFT CHC
Note : The FWD CHC and AFT CHC pages are optional.
LAST LEG CLASS 3 FAULTS
This item presents the class 3 failures concerning
　
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