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the following cabin systems :
‐ Cabin and service interphone
‐ Passenger address
‐ Passenger lighted signs
‐ Reading lights (LED technology)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
INTERCOMMUNICATION SYSTEMS - GENERAL
A318/A319/A320/A321 FLEET DSC-23-20-10 P 7/10
FCOM 19 AUG 10
‐ General cabin illumination
‐ Emergency evacuation signalling
‐ Lavatory smoke detectors and indicators
‐ Passenger entertainment music and video
‐ Escape slide bottle pressure monitoring
‐ Vacuum system control function
‐ Cargo and lavatory smoke detection function
The CIDS has the following main components :
‐ Two CIDS directors connected in parallel ; one active, and the other on standby.
‐ Flight Attendant Panel (FAP) to monitor and control the cabin systems.
‐ Attendant Indication Panels (AIP), After Attendant Panels (AAP) and Area Call Panels (ACP)
‐ Decoder/Encoder Units (DEUs) linked to the two directors.
• Type A units (for passengers) installed along the cabin.
The loudspeakers, lighted signs, call buttons, call lights and general illumination ballast units are
divided into small groups, each connected to a type A DEU.
• Type B units (for attendants) installed near the exit doors. The Area Call panels, smoke
detectors, attendant handsets, slide and door pressure sensors, and attendant indicator panels,
are connected to type B DEUs.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
INTERCOMMUNICATION SYSTEMS - GENERAL
A318/A319/A320/A321 FLEET DSC-23-20-10 P 8/10
FCOM 19 AUG 10
CABIN INTERCOMMUNICATION DATA SYSTEM
Applicable to:
The Cabin Intercommunication Data System (CIDS) transmits, controls, and processes signals for
the following cabin systems :
‐ Cabin and service interphone
‐ Passenger address
‐ Passenger lighted signs
‐ Reading lights
‐ General cabin illumination
‐ Emergency evacuation signalling
‐ Lavatory smoke indicators
‐ Passenger entertainment music and video
‐ Escape slide bottle pressure monitoring
The CIDS has the following main components :
‐ Two CIDS directors connected in parallel ; one active, and the other on standby.
‐ Forward attendant panel for control of the cabin systems.
‐ Programming and test module that allows the system to be reprogrammed after changes are
made in the cabin configuration.
‐ Decoder/Encoder Units (DEUs) linked to the two directors.
• Type A units (for passengers) installed along the cabin.
The loudspeakers, lighted signs, call buttons, call lights and general illumination ballast units are
divided into small groups, each connected to a type A DEU.
• Type B units (for attendants) installed near the exit doors. The Area Call panels, attendant
handsets, slide and door pressure sensors, and attendant indicator panels, are connected to
type B DEUs.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
INTERCOMMUNICATION SYSTEMS - GENERAL
A318/A319/A320/A321 FLEET DSC-23-20-10 P 9/10
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
INTERCOMMUNICATION SYSTEMS - GENERAL
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A318/A319/A320/A321 FLEET DSC-23-20-10 P 10/10
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
INTERCOMMUNICATION SYSTEMS - CONTROLS
A318/A319/A320/A321 FLEET DSC-23-20-20 P 1/12
FCOM 19 AUG 10
AUDIO CONTROL PANEL
Applicable to:
(1) Transmission keys
Pressed : The associated channel is selected for transmission.
The three green lines come on.
The pilot deselects the channel by pressing the pushbutton again, or
selecting another channel.
CALL : The legend flashes in amber (and the buzzer sounds), when the SELCAL
system detects a call.
MECH : The legend flashes in amber (and the buzzer sounds), for a call from the
nose gear bay. The MECH light goes off after 60 s, if it is not reset.
ATT : The legend flashes in amber (and the buzzer sounds), for a call from a cabin
crewmember. The ATT light goes off after 60 s, if it is not reset.
(2) Reception knobs
These knobs allow the flight crew to select reception channels and to adjust their volume.
‐ Pressing and releasing the knob (knob out) selects the associated audio reception channel.
The integral white light comes on. Rotating the knob adjusts the volume.
‐ Pressing the knob (knob stays in) disconnects the associated audio reception channel.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 2(134)
