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EFFECTIVITY 23-71-00 Page 2
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 168
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - IN FLIGHT
TMUCOMS01-P01 LEVEL 3
EFFECTIVITY 23-71-00 Page 3
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 169
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
ON GROUND
The CVR is automatically supplied when the aircraft
is on ground with one or both engines running.
TMUCOMS01-T02 LEVEL 3
EFFECTIVITY 23-71-00 Page 4
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 170
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - ON GROUND (1/3)
TMUCOMS01-P02 LEVEL 3
EFFECTIVITY 23-71-00 Page 5
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 171
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
The CVR continues running up to five minutes after 2nd
engine shutdown.
TMUCOMS01-T03 LEVEL 3
EFFECTIVITY 23-71-00 Page 6
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 172
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - ON GROUND (2/3)
TMUCOMS01-P03 LEVEL 3
EFFECTIVITY 23-71-00 Page 7
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 173
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
Five minutes after the second engine shutdown, the
supply of the CVR is automatically cut off.
TMUCOMS01-T04 LEVEL 3
EFFECTIVITY 23-71-00 Page 8
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 174
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - ON GROUND (3/3)
TMUCOMS01-P04 LEVEL 3
EFFECTIVITY 23-71-00 Page 9
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 175
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
MANUAL MODE
On ground, engines shut down, the cockpit voice
recorder may be energized by pressing the GND/CTL
pushbutton on the RCDR panel.
The GND/CTL pushbutton is a momentary type switch.
When RCDR/GND CTL pushbutton is pressed, relay 12 TU
is energized and held energized. This also energizes
the relay 6 RK which enables the CVR to be supplied.
TMUCOMS01-T05 LEVEL 3
EFFECTIVITY 23-71-00 Page 10
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 176
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - MANUAL MODE (1/5)
TMUCOMS01-P05 LEVEL 3
EFFECTIVITY 23-71-00 Page 11
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 177
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
Then released, the relays 12 TU and 6 RK remain
energized but in addition the relay 13 TU is energized.
TMUCOMS01-T06 LEVEL 3
EFFECTIVITY 23-71-00 Page 12
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 178
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - MANUAL MODE (2/5)
TMUCOMS01-P06 LEVEL 3
EFFECTIVITY 23-71-00 Page 13
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 179
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC
Pressed again, the supplies of the relay 12 TU and 6
RK are cut off simultaneously, the blue ON light goes
off and the CVR is no longer supplied.
TMUCOMS01-T07 LEVEL 3
EFFECTIVITY 23-71-00 Page 14
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 180
ALL
COCKPIT VOICE RECORDER ELECTRICAL SCHEMATIC - MANUAL MODE (3/5)
TMUCOMS01-P07 LEVEL 3
EFFECTIVITY 23-71-00 Page 15
　
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