R 1EFF : 001-049, 051-099, 101-105, 201-299, 1 23-73-00Page 518 1 1 May 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------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 RETURN related pushbutton switch.

 -
push the GND SCAN related pushbutton switch.

-
push the MCDU MENU pushbutton switch.

 **ON A/C 151-199,
 Subtask 23-73-00-740-053-A
 A. Do this test.
-
the CIDS1 (ACT) page comes on.

-
the CIDS1 (ACT) GROUND SCANNING pagewith NO FAILURE message comes on.

-
the MCDU MENU page comes on.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the C/B panel 49VU:

 - open the C/Bs DIR ESS/1 and DIR ESS/2 150RH and 157RH.

 2.
 On the C/B panel 121VU:

- open the C/Bs DIR NORM/1 and DIR NORM/2 151RH and 156RH.
On the Forward Attendant Panel (FAP) 120RH:
-
the CIDS CAUT light comes on.

 On the PTP 110RH:

 -
the message CIDS DEGRADATION comes on.

 In the cockpit on the UPPER ECAM DISPLAY:

 -
the message COM CIDS 1+2 FAULT comes on.

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 23-73-00Page 519 1201-299, 1May 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
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 loudspeakers: - a single chime is heard.
 3. On the ECAM Control-Panel (ECP): - push the STS pushbutton.  On the LOWER ECAM DISPLAY:- the message INOP SYS CIDS comes on.
 4. On the C/B panel 121VU: - after approx. 10 s close the C/Bs DIR NORM/1 and DIR NORM/2 151RH and 156RH.
 5. On the C/B panel 49VU:
 - close the C/Bs DIR ESS/1 and DIR ESS/2 150RH and 157RH. - the CIDS CAUT light goes off.

 NOTE : Wait approx. 5 minutes before you start the next test step.
____
 - after approx. 5 minutes the CIDS CAUT light stays off.
 In the cockpit on the UPPER and LOWER ECAM DISPLAY: - all the CIDS FAULT messages are off.
 ON the PTP: - the SYSTEM STATUS page and the message CIDS OK come on.
 6. On the CFDS-MCDU:  On the CFDS-MCDU:
 - push the MCDU MENU pushbutton switch. - the MCDU MENU page comes on.
 - push the CFDS related pushbutton switch.  - the CFDS page comes on.

R 1EFF : 151-199, 1 23-73-00Page 520 1 1 Feb 01/03 1 1 1CES 1

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- push the SYSTEM REPORT/TEST  - the SYSTEM REPORT/TEST page comes on.
 pushbutton switch.
 - push the COM related pushbutton  - the SYSTEM REPORT/TEST COM page comes
 switch.  on.
 - push the CIDS1 related  - the CIDS1 (ACT) page comes on.
 pushbutton switch.
 - push the CLASS 3 FAULTS related  - the CIDS1 (ACT) CLASS 3 FAULTS page
 pushbutton switch.  with NO FAILURE message 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 RETURN related  - the CIDS1 (ACT) page comes on.
 pushbutton switch.
 - push the GND SCAN related  - the CIDS1 (ACT) GROUND SCANNING page
 pushbutton switch.  with NO FAILURE message comes on.
 - push the MCDU MENU pushbutton  - the MCDU MENU page comes on.
 switch. 

R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
R  5. Close-up________ **ON A/C 001-049, 051-056, 101-101,
 Subtask 23-73-00-860-088
 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 aircraft electrical circuits (Ref. TASK 24-41-00-862-002) 
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM Communications 通訊3(141)