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Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
Then released again, the relay 13 TU is de-energized.
TMUCOMS01-T08 LEVEL 3
EFFECTIVITY 23-71-00 Page 16
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UF94200
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COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - MANUAL MODE (4/5)
TMUCOMS01-P08 LEVEL 3
EFFECTIVITY 23-71-00 Page 17
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COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
If one engine is started, the CVR is automatically
supplied.
TMUCOMS01-T09 LEVEL 3
EFFECTIVITY 23-71-00 Page 18
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - MANUAL MODE (5/5)
TMUCOMS01-P09 LEVEL 3
EFFECTIVITY 23-71-00 Page 19
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SELF EXAMINATION
When is the CVR energized with the aircraft on
ground and engines shut down ?
A - When the parking brake is applied.
B - During 5 minutes after the second engine
is shut down.
C - When CVR TEST pushbutton is pressed.
TMUCOMS01 LEVEL 3
EFFECTIVITY 23-71-00 Page 20
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23 - COMMUNICATIONS
23-71-00 COCKPIT VOICE RECORDER COMPONENTS
CONTENTS:
Cockpit Voice Recorder (CVR)
RCDR Panel
CVR Head Set Jack
TMUCOMZ01 LEVEL 3
EFFECTIVITY 23-71-00 Page 1
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
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UF94200
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COCKPIT VOICE RECORDER COMPONENTS
COCKPIT VOICE RECORDER (CVR)
IDENTIFICATION
FIN : 1RK
LOCATION
ZONE : 312
TMUCOMZ01-T01 LEVEL 3
EFFECTIVITY 23-71-00 Page 2
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TMUCOMZ01-P01 LEVEL 3
COCKPIT VOICE RECORDER COMPONENTS - CVR
EFFECTIVITY 23-71-00 Page 3
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COCKPIT VOICE RECORDER COMPONENTS
RCDR PANEL
IDENTIFICATION
FIN : 11TU, 3RK, 5RK
LOCATION
ZONE : 211
CVR HEAD SET JACK
IDENTIFICATION
FIN : 22RK
LOCATION
ZONE : 210
TMUCOMZ01-T02 LEVEL 3
EFFECTIVITY 23-71-00 Page 4
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COCKPIT VOICE RECORDER COMPONENTS - CVR
HEAD SET JACK
TMUCOMZ01-P02 LEVEL 3
COCKPIT VOICE RECORDER COMPONENTS - RCDR
PANEL
EFFECTIVITY 23-71-00 Page 5
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUCOMZ01 LEVEL 3
EFFECTIVITY 23-71-00 Page 6
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23 - COMMUNICATIONS
23-73-00 CABIN INTERCOMMUNICATION DATA
SYSTEM DESIGN PHILOSOPHY
CONTENTS:
General
Principle
Passengers Functions
Crew Functions
Cabin Systems Functions
Monitoring And Test Functions
Aircraft Systems Functions
Cockpit Controls And Indicating
TMUCI2A02 LEVEL 1
EFFECTIVITY 23-73-00 Page 1
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CABIN INTERCOMMUNICATION DATA SYSTEM DESIGN PHILOSOPHY
GENERAL
Changing market demands require flexibility in
　
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