In the cockpit on the UPPER ECAM DISPLAY:
-
the message COM CIDS 1+2 FAULT comes on.
NOTE : To show all of the message, you
____ have to clear all other ECAM warnings. To clear all other ECAM warnings push the CLR pushbutton on the ECAM Control-Panel (ECP), until all of the COM message appears.
Through the cockpit loudspeaker:
-a single chime is heard.
On the LOWER ECAM DISPLAY:
-
the message INOP SYS CIDS comes on.
-
the CIDS CAUT light goes off.
NOTE : Wait approx. 5 min before you start the next test step.
____
-after approx. 5 min the CIDS CAUT light is still off.
In the cockpit on the UPPER and LOWER ECAM DISPLAY:
-all CIDS FAULT messages are off.
6. On the Programming and Test Panel On the PTP 110RH: (PTP) 110RH:
1EFF : 151-199, 1 23-73-00Page 509 1 1 May 01/05R 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- push the DSPL ON membrane - the CIDS menu page comes on.
switch.
- push the SYSTEM STATUS related - the SYSTEM STATUS page comes on with
membrane switch. system OK messages.
- push the CONT related membrane - the next system status related pages
switch until the < MAINTENANCE with system OK messages come on.
message comes on.
- push the MAINTENANCE related - the MAINTENANCE page comes on.
membrane switch.
- push the CONT related membrane
switch until the < GND SCAN
message comes on.
- push the GND SCAN related - the GND SCAN page with the NO FAILURE
membrane switch. message comes on.
- push the RET related membrane - the SYSTEM STATUS page comes on.
switch until the SYSTEM STATUS
page comes on.
- push the CONT related membrane
switch until the < MAINTENANCE
message comes on.
- push the MAINTENANCE related - the MAINTENANCE page comes on.
membrane switch.
- push the CONT related membrane - the < CLASS 3 FAULTS message comes
switch. on.
- push the < CLASS 3 FAULTS - the CLASS 3 FAULT page with NO
related membrane switch. FAILURE messages comes on.
NOTE : An erroneous class 3 fault message will be recorded for each LED
____ (without bulbs) Cabin Sign; if the test of the related signs is not deactivated in the CAM.
-push the DSPL ON membrane - the CIDS menu page comes on. switch.
R 1EFF : 151-199, 1 23-73-00Page 510 1 1 May 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
5. Close-up________
R **ON A/C 001-049, 051-056, 101-101,
Subtask 23-73-00-860-084
A. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002)
(2) De-energize the CFDS (Ref. TASK 31-32-00-860-003).
(3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002)
R **ON A/C 001-049, 057-099, 101-105, 151-199, 201-299,
R Post SB 23-1121 For A/C 001-049,101-101,
Subtask 23-73-00-860-084-A
A. Put the aircraft back to its initial configuration.
NOTE : If some reading lights be inoperational after the test:____ - switch off the reading lights on the FAP 120RH for approx. 10 sec. and than on again.
NOTE : If the NS signs in a Non Smoker A/C configuration do not come on:____ - set the NS switch to the AUTO or ON position and than back again.
(1) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002)
(2) De-energize the CFDS (Ref. TASK 31-32-00-860-003).
(3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002)
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page 511 1201-299, 1May 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
TASK 23-73-00-740-005
BITE Test of the Cabin Intercommunication Data System (CIDS) through the CFDS
1. Reason for the Job
__________________
Reset and BITE Test of the CIDS.
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