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┃I ~-~ A318 ┃I INTERCOMMUNICATION SYSTEMS ┃SEQ 001 1 ┃I REV 28 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
CABIN INTERCOMMUNICATION DATA SYSTEM
The Cabin Intercommunication Data System (CIDS) transmits, controls, and processes
signals for the following cabin systems :
- cabin and service interphone
- passenger address
- passenger lighted sign
- reading light
- general cabin illumination
- emergency evacuation signalling
- lavatory smoke indication
- 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 in 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.
COCKPIT
FUNCTTONS
PASSENGER
FUNCTIONS
CABIN ATTN
FUNCTIONS
Becoder/Encoder Units (DEUs) are linked to the two directors~
~ Type A units (for passengers) are along each side of the passenger 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) are 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.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃I -~ A318 ┃ COMMUNICATIONS ┃1.23.20 P 5 ┃
┃ ,imam ,, ~4W~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 100 I ┃I REV 35 ┃
┃ A~7-~'M" A321 ┃INTERCOMMUNICATION SYSTEMS ┃ ┃ ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual2(125)
