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PASSENGER VISUAL INFORMATION SYSTEM COMPONENTS - DIGITAL INTERFACE UNIT
TMU23EJ01-P01 LEVEL 3
EFFECTIVITY 23-34-00 Page 3
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 427
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PASSENGER VISUAL INFORMATION SYSTEM COMPONENTS
REMOTE CONTROL UNIT
IDENTIFICATION
FIN: 191MH
LOCATION
ZONE: 230
TMU23EJ01-T02 LEVEL 3
EFFECTIVITY 23-34-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
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PASSENGER VISUAL INFORMATION SYSTEM COMPONENTS - REMOTE CONTROL UNIT
TMU23EJ01-P02 LEVEL 3
EFFECTIVITY 23-34-00 Page 5
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
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TMU23EJ01 LEVEL 3
EFFECTIVITY 23-34-00 Page 6
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 430
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23 - COMMUNICATIONS
23-74-00 CABIN MANAGEMENT SYSTEM
DESCRIPTION AND OPERATION
CONTENTS:
CMS
CMS Components
Operation
Test
TMU23EM02 LEVEL 3
EFFECTIVITY 23-74-00 Page 1
Jun 30/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 431
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CABIN MANAGEMENT SYSTEM DESCRIPTION AND OPERATION
CMS
The Cabin Management System (CMS) provides a direct
contact for the cabin crew with the ground via the Air
Traffic Service Unit (ATSU).
Transmitted data can be passenger and security
information or maintenance reports.
CMS COMPONENTS
The CMS is composed of:
- a laptop computer,
- a dot matrix printer,
- an interface assembly,
- a message awaiting light.
The interface is provided with two sliding drawers
(one for the computer and one for the printer). It is
also equipped with a power supply circuit board and
an interface circuit board.
The message awaiting light indicates that information
has been received from a ground station.
OPERATION
All system controls and data entries are made on the
laptop computer.
The software provides guidance for the operator to use
the system.
All functions are available through selection from the
display.
To operate the CMS, first the printer drawer has to
be unlocked and pulled forward then pushed back to the
locked position.
After that, the computer drawer has to be unlocked and
pulled forward.
Then the computer can be switched on.
TEST
The CMS has Built-In Test Equipment (BITE). The test
is done when the system is powered-up.
TMU23EM02-T01 LEVEL 3
EFFECTIVITY 23-74-00 Page 2
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MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
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CABIN MANAGEMENT SYSTEM DESCRIPTION AND OPERATION - SCHEMATIC
TMU23EM02-P01 LEVEL 3
EFFECTIVITY 23-74-00 Page 3
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TMU23EM02 LEVEL 3
EFFECTIVITY 23-74-00 Page 4
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UF94200
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23 - COMMUNICATIONS
23-74-00 CABIN MANAGEMENT SYSTEM
COMPONENTS
CONTENTS:
Cabin Management System
Message Awaiting Light
TMU23EN01 LEVEL 3
EFFECTIVITY 23-74-00 Page 1
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
EFFECTIVITY Page 435
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CABIN MANAGEMENT SYSTEM COMPONENTS
CABIN MANAGEMENT SYSTEM
IDENTIFICATION
FIN: 2RF
LOCATION
ZONE: 221
NOTE
Depending on the airline’s choice, the Cabin Management
Terminal can be installed without the printer in the
entrance area.
TMU23EN01-T01 LEVEL 3
EFFECTIVITY 23-74-00 Page 2
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 23 COMMUNICATIONS
UF94200
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CABIN MANAGEMENT SYSTEM COMPONENTS - CABIN MANAGEMENT SYSTEM
　
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